SIGI, 62632
Orbit data source: Space-Track
SIGI, 62632 is a German payload satellite in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62632 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
REFLEX
Mission
Operational Commercial Communications
Bus & Motor
OMNIFLEX, Unknown motor
Mass
109 kg wet, 109 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
1.176 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SIGI
1 62632U 25009Z 26215.90220725 .00005700 00000-0 23046-3 0 9998
2 62632 97.3982 295.5341 0004580 127.9824 232.1828 15.25112962 86079Epoch: 2026-08-03T21:39Z
TLE epoch observation values (Epoch: 2026-08-03T21:39:10.706Z)
Latitude
-0.00003°
Longitude
18.26084°
Altitude
495.474 km
Speed
7.616 km/s
True Right ascension
19h 42m 08s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
18:59:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.549 km
Perigee altitude
484.261 km
Semi-major axis
6,865.542 km
Eccentricity
0.00046
Inclination
97.3982°
RAAN
295.5341°
Arg. of periapsis
127.9824°
True anomaly
232.14135°
Mean anomaly
232.1828°
Eccentric anomaly
232.16208°
Mean motion
3.81532 °/min
Orbital period
94.36 mins
BSTAR
0.00023046
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SIGI Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-05 05:16:04.228Z | 158.786° S | 2026-08-05 05:19:04.228Z | 116.004° SE | 41.7° | 2026-08-05 05:22:04.228Z | 355.374° N |
| 5 mins | 2026-08-05 18:19:04.228Z | 7.941° NNE | 2026-08-05 18:21:04.228Z | 311.98° NW | 44.495° | 2026-08-05 18:24:04.228Z | 196.878° SSW |
| 5 mins | 2026-08-06 04:55:04.228Z | 123.049° SE | 2026-08-06 04:57:04.228Z | 66.039° ENE | 28.617° | 2026-08-06 05:00:04.228Z | 8.065° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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