MR-2, 67556
Orbit data source: Space-Track
MR-2, 67556 is a payload satellite owned by Open Cosmos (ES) in LEO that was launched on Thu, 22 Jan 2026 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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67556 intel report (Beta)
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Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
Open Cosmos
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 12U?, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 MR-2
1 67556U 26015A 26171.31007227 .00000051 00000-0 59175-4 0 9999
2 67556 89.0005 268.2214 0005240 80.5177 279.6567 13.52694656 20132Epoch: 2026-06-20T07:26Z
TLE epoch observation values (Epoch: 2026-06-20T07:26:30.244Z)
Latitude
-0.00002°
Longitude
-111.93115°
Altitude
1,064.664 km
Speed
7.32 km/s
True Right ascension
17h 52m 53s
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
07:24:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,063.307 km
Perigee altitude
1,055.512 km
Semi-major axis
7,437.546 km
Eccentricity
0.00052
Inclination
89.0005°
RAAN
268.2214°
Arg. of periapsis
80.5177°
True anomaly
279.5975°
Mean anomaly
279.6567°
Eccentric anomaly
279.6271°
Mean motion
3.38375 °/min
Orbital period
106.39 mins
BSTAR
0.000059175
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Other satellites on launch #15 in the year 2026 (2026-01-22 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.MR-2 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 | 2026-06-20 20:29:49.237Z | 314.736° NW | 2026-06-20 20:32:49.237Z | 285.18° WNW | 14.889° | 2026-06-20 20:35:49.237Z | 257.002° W |
| 11 mins | 2026-06-21 06:37:49.237Z | 165.742° S | 2026-06-21 06:42:49.237Z | 100.591° ESE | 43.101° | 2026-06-21 06:48:49.237Z | 4.867° NNE |
| 7 mins | 2026-06-21 08:26:49.237Z | 250.34° W | 2026-06-21 08:29:49.237Z | 280.746° WNW | 17.071° | 2026-06-21 08:33:49.237Z | 320.67° NNW |
| 10 mins | 2026-06-21 17:46:49.237Z | 25.769° NE | 2026-06-21 17:51:49.237Z | 87.158° E | 28.381° | 2026-06-21 17:56:49.237Z | 142.161° SSE |
| 10 mins | 2026-06-21 19:33:49.237Z | 336.24° NNW | 2026-06-21 19:37:49.237Z | 282.549° WNW | 31.967° | 2026-06-21 19:43:49.237Z | 214.626° SW |
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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