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 57204U 26145.55924801 +.00000000 +00000-0 +51778-3 0 00004
2 57204 97.5103 215.7764 0007922 141.4925 218.6886 15.37444548 07
| Epoch (UTC): | 25 May 2026 13:25:19 |
| Eccentricity: | 0.0007922 |
| inclination: | 97.5103° |
| perigee height: | 448 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 215.7764° |
| argument of perigee: | 141.4925° |
| revolutions per day: | 15.37444548 |
| mean anomaly at epoch: | 218.6886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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