Skip to content
SatelliteIndex

Satellite · NORAD 42760 · COSPAR 2017-034C

NUSAT-3 (MILANESAT)

DecayedPayloadLEOEarth observation derived

Altitude now

—

object decayed

Velocity

—

Inclination

42.97°

Period

88.1 min

88.1 min

Perigee

176km

Apogee

179km

orbit unavailableNo orbital element set on file — decayed 22 Jun 2025.· Metadata updated 8 h ago

Live position

Live position

Live position unavailable — this object re-entered the atmosphere on 22 Jun 2025 and is no longer tracked.

Mission

Mission & classification

Mission type derived
Earth observation
Object type
Payload
SATCAT ops status
Decayed [D]
Radar cross-section
—
Constellation membership derived
Satellogic NewSat (Ñusat) via name_pattern

CelesTrak groups

Not listed in any CelesTrak group.

Aliases

  • NUSAT-3 (MILANESAT)Celestrak Satcat

Ownership

Operator & country

Operator
Satellogic
SATCAT owner code
ARGN · Argentina
Country
Argentina AR

Launch

Launch

Launch page →
Launch date
15 Jun 2017
COSPAR launch id
2017-034
Launch site
Jiuquan Satellite Launch Center

Objects from the same launch · 6

Change log

History

No changes recorded since first ingestion on 11 Sept 2026 18:54 UTC. Status, orbit class, name and ownership changes are logged here as sources are re-ingested.

Regulatory

UN registration

UN Register of Objects Launched into Outer Space (UNOOSA) — connector planned, not yet ingested; registration unavailable

Transparency

Sources & provenance

All sources →

No source is linked to this record yet — the catalogue row exists but no provenance entry has been written for it.

Field provenance

No field-level provenance recorded.

Timeline

Events

All events →

No events detected for this object yet. Launches, decays and orbit changes are generated by the derived-analytics connector.

Reference

Identifiers

NORAD catalogue number
42760
COSPAR / international designator
2017-034C
SatelliteIndex id
sat_01M28X3JTYYCTRKZHTWC1VGP54
Canonical slug
nusat-3-milanesat-42760

Orbit class, mission type and constellation membership are derived by SatelliteIndex (Earth observation) — see the methodology. Positions are propagated estimates, not tracking measurements; never use them for conjunction assessment.