OT-FOREST-17 TELPERION, 68988
Orbit data source: Space-Track
OT-FOREST-17 TELPERION, 68988 is a German payload satellite in SSO that was launched on Sun, 03 May 2026 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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68988 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
OroraTech
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
~15 kg wet, ~15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OT-FOREST-17 TELPERION
1 68988U 26100J 26266.15460712 .00000641 00000-0 67185-4 0 9998
2 68988 97.7205 161.6446 0005700 160.6923 199.4513 14.92923308 21307Epoch: 2026-09-23T03:42Z
TLE epoch observation values (Epoch: 2026-09-23T03:42:38.055Z)
Latitude
-0.00005°
Longitude
103.97624°
Altitude
595.616 km
Speed
7.56 km/s
True Right ascension
10h 46m 34s
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
04:07:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.811 km
Perigee altitude
581.872 km
Semi-major axis
6,963.979 km
Eccentricity
0.00057
Inclination
97.7205°
RAAN
161.6446°
Arg. of periapsis
160.6923°
True anomaly
199.42956°
Mean anomaly
199.4513°
Eccentric anomaly
199.44043°
Mean motion
3.73471 °/min
Orbital period
96.39 mins
BSTAR
0.000067185
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Other satellites on launch #100 in the year 2026 (2026-05-03 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.OT-FOREST-17 TELPERION 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-23 16:42:06.569Z | 142.858° SSE | 2026-09-23 16:46:06.569Z | 63.498° ENE | 42.095° | 2026-09-23 16:49:06.569Z | 5.692° NNE |
| 6 mins | 2026-09-24 06:02:06.569Z | 13.247° NNE | 2026-09-24 06:04:06.569Z | 21.454° NNE | 81.243° | 2026-09-24 06:08:06.569Z | 192.958° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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