DOJO, 65302
Orbit data source: Space-Track
DOJO, 65302 is a payload satellite owned by E-Space (RW) in SSO that was launched on Sat, 23 Aug 2025 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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65302 intel report (Beta)
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Identifier
Orbit
Country
RW / RWARelated business
Manufacturer
E-Space
Mission
Operational Commercial Communications
Bus & Motor
CALISTUS, Unknown motor
Mass
~30 kg wet, ~30 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 1.1 m
Radar Cross Section
0.475 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 DOJO
1 65302U 25185F 26162.79767701 .00010408 00000-0 14030-2 0 9991
2 65302 97.9653 246.2327 0015629 106.0356 254.2578 14.79254810 43042Epoch: 2026-06-11T19:08Z
TLE epoch observation values (Epoch: 2026-06-11T19:08:39.293Z)
Latitude
-0.00002°
Longitude
58.93267°
Altitude
637.685 km
Speed
7.538 km/s
True Right ascension
16h 24m 55s
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
11:32:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
639.673 km
Perigee altitude
617.771 km
Semi-major axis
7,006.859 km
Eccentricity
0.00156
Inclination
97.9653°
RAAN
246.2327°
Arg. of periapsis
106.0356°
True anomaly
254.08551°
Mean anomaly
254.2578°
Eccentric anomaly
254.17165°
Mean motion
3.70048 °/min
Orbital period
97.28 mins
BSTAR
0.001403
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Other satellites on launch #185 in the year 2025 (2025-08-23 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.DOJO 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 | 2026-06-12 05:01:04.635Z | 134.891° SE | 2026-06-12 05:04:04.635Z | 84.048° E | 30.815° | 2026-06-12 05:08:04.635Z | 6.241° NNE |
| 4 mins | 2026-06-12 06:39:04.635Z | 236.543° WSW | 2026-06-12 06:41:04.635Z | 269.676° W | 17.183° | 2026-06-12 06:43:04.635Z | 301.165° NW |
| 7 mins | 2026-06-12 18:27:04.635Z | 14.165° NNE | 2026-06-12 18:30:04.635Z | 141.334° SSE | 44.909° | 2026-06-12 18:34:04.635Z | 192.43° SSW |
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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