View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 57903U 26145.61994022 +.00000000 +00000-0 +90692-6 0 00000
2 57903 42.9996 239.5717 0001181 275.9431 84.1286 15.27574400 05
| Epoch (UTC): | 25 May 2026 14:52:42 |
| Eccentricity: | 0.0001181 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 239.5717° |
| argument of perigee: | 275.9431° |
| revolutions per day: | 15.27574400 |
| mean anomaly at epoch: | 84.1286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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