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 57202U 26145.61273448 +.00000000 +00000-0 +21120-3 0 00001
2 57202 97.5130 204.5505 0009689 178.1081 182.0191 15.18868885 02
| Epoch (UTC): | 25 May 2026 14:42:20 |
| Eccentricity: | 0.0009689 |
| inclination: | 97.5130° |
| perigee height: | 503 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 204.5505° |
| argument of perigee: | 178.1081° |
| revolutions per day: | 15.18868885 |
| mean anomaly at epoch: | 182.0191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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