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 57973U 26145.62491913 +.00000000 +00000-0 +11872-4 0 00000
2 57973 43.0020 261.4193 0001234 278.8236 81.2476 15.27581503 09
| Epoch (UTC): | 25 May 2026 14:59:53 |
| Eccentricity: | 0.0001234 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 261.4193° |
| argument of perigee: | 278.8236° |
| revolutions per day: | 15.27581503 |
| mean anomaly at epoch: | 81.2476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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