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 57990U 26145.50265505 +.00000000 +00000-0 +20732-3 0 00006
2 57990 34.9906 77.5913 0011122 295.3741 64.5820 15.17757917 08
| Epoch (UTC): | 25 May 2026 12:03:49 |
| Eccentricity: | 0.0011122 |
| inclination: | 34.9906° |
| perigee height: | 505 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 77.5913° |
| argument of perigee: | 295.3741° |
| revolutions per day: | 15.17757917 |
| mean anomaly at epoch: | 64.5820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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