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 57908U 26145.27081330 +.00000000 +00000-0 +72477-4 0 00005
2 57908 43.0042 245.5090 0001880 266.9408 93.1229 15.27581664 02
| Epoch (UTC): | 25 May 2026 06:29:58 |
| Eccentricity: | 0.0001880 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 245.5090° |
| argument of perigee: | 266.9408° |
| revolutions per day: | 15.27581664 |
| mean anomaly at epoch: | 93.1229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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