IMPULSE-2 MIRA, 62673
Orbit data source: Space-Track
IMPULSE-2 MIRA, 62673 is a payload satellite owned by Impulse Space (US) 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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62673 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Impulse Space
Mission
Operational Commercial Technology
Bus & Motor
MIRA, AOCS
Mass
250 kg wet, 200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.2 m
Radar Cross Section
0.575 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 IMPULSE-2 MIRA
1 62673U 25009BS 25286.18237268 .00012183 00000-0 40651-3 0 9994
2 62673 97.5416 2.6923 0085211 278.5940 80.5651 15.27711357 98878Epoch: 2025-10-13T04:22Z
TLE epoch observation values (Epoch: 2025-10-13T04:22:36.999Z)
Latitude
-0.00005°
Longitude
-84.95068°
Altitude
476.653 km
Speed
7.632 km/s
True Right ascension
00h 10m 46s
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
18:51:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.053 km
Perigee altitude
421.181 km
Semi-major axis
6,857.754 km
Eccentricity
0.00852
Inclination
97.5416°
RAAN
2.6923°
Arg. of periapsis
278.594°
True anomaly
81.52998°
Mean anomaly
80.5651°
Eccentric anomaly
81.04738°
Mean motion
3.82182 °/min
Orbital period
94.2 mins
BSTAR
0.00040651
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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.IMPULSE-2 MIRA 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-14 05:39:52.084Z | 199.269° SSW | 2025-10-14 05:41:52.084Z | 251.997° W | 33.565° | 2025-10-14 05:44:52.084Z | 328.655° NNW |
| 5 mins | 2025-10-14 18:40:52.084Z | 337.127° NNW | 2025-10-14 18:42:52.084Z | 285.352° WNW | 28.045° | 2025-10-14 18:45:52.084Z | 226.549° WSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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