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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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: 7 hours ago
TLE from 7 hours ago
0 IMPULSE-2 MIRA
1 62673U 25009BS 26125.09253184 .00009131 00000-0 35023-3 0 9998
2 62673 96.6243 199.9837 0009586 166.7731 193.3762 15.26634299130025Epoch: 2026-05-05T02:13Z
TLE epoch observation values (Epoch: 2026-05-05T02:13:14.750Z)
Latitude
-0.00015°
Longitude
-56.30008°
Altitude
495.406 km
Speed
7.613 km/s
True Right ascension
13h 19m 56s
True Declination
0° 00' 01"
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
16:46:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.384 km
Perigee altitude
476.231 km
Semi-major axis
6,860.945 km
Eccentricity
0.00096
Inclination
96.6243°
RAAN
199.9837°
Arg. of periapsis
166.7731°
True anomaly
193.35082°
Mean anomaly
193.3762°
Eccentric anomaly
193.36351°
Mean motion
3.81916 °/min
Orbital period
94.26 mins
BSTAR
0.00035023
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-05 16:57:44.786Z | 55.658° ENE | 2026-05-05 16:59:44.786Z | 95.098° ESE | 17.392° | 2026-05-05 17:01:44.786Z | 133.302° SE |
| 4 mins | 2026-05-05 18:31:44.786Z | 323.005° NNW | 2026-05-05 18:32:44.786Z | 300.101° NW | 21.241° | 2026-05-05 18:35:44.786Z | 237.182° WSW |
| 6 mins | 2026-05-06 05:05:44.786Z | 171.25° S | 2026-05-06 05:08:44.786Z | 332.782° NNW | 42.705° | 2026-05-06 05:11:44.786Z | 347.495° N |
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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