Satellite · NORAD 41558 · COSPAR 2016-033C
NUSAT-2 (BATATA)
- Operator Satellogic
- Constellation Satellogic NewSat (Ñusat)
- Country Argentina
Altitude now
—
object decayed
Velocity
—
Inclination
97.41°
Period
87.3 min
87.3 min
Perigee
132km
Apogee
146km
orbit unavailableNo orbital element set on file — decayed 04 Oct 2023.· Metadata updated 8 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 04 Oct 2023 and is no longer tracked.
Mission
Mission & classification
- Mission type derived
- Earth observation
- Object type
- Payload
- SATCAT ops status
- Decayed [D]
- Radar cross-section
- 0.3 m²
- Constellation membership derived
- Satellogic NewSat (Ñusat) via name_pattern
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- NUSAT-2 (BATATA)Celestrak Satcat
Ownership
Operator & country
- Operator
- Satellogic
- SATCAT owner code
- ARGN · Argentina
- Country
- Argentina AR
Launch
Launch
- Launch date
- 30 May 2016
- COSPAR launch id
- 2016-033
- Launch site
- Taiyuan Satellite Launch Center
Objects from the same launch · 4
- NUSAT 1 DEB43427DebrisDecayed
- ZIYUAN 3-02 (ZY 3-02)41556PayloadActive
- NUSAT-1 (FRESCO)41557PayloadDecayed
- CZ-4B R/B41559Rocket bodyDecayed
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
Transparency
Sources & provenance
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
No events detected for this object yet. Launches, decays and orbit changes are generated by the derived-analytics connector.
Reference
Identifiers
- NORAD catalogue number
- 41558
- COSPAR / international designator
- 2016-033C
- SatelliteIndex id
- sat_01M28X3JTR27RWATBPVQ3JHQPZ
- Canonical slug
- nusat-2-batata-41558
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.