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 57988U 26145.50640671 +.00000000 +00000-0 +30377-3 0 00000
2 57988 34.9904 77.6499 0019205 22.8758 337.2807 15.17711336 04
| Epoch (UTC): | 25 May 2026 12:09:13 |
| Eccentricity: | 0.0019205 |
| inclination: | 34.9904° |
| perigee height: | 500 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 77.6499° |
| argument of perigee: | 22.8758° |
| revolutions per day: | 15.17711336 |
| mean anomaly at epoch: | 337.2807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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