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 57854U 26145.12073041 +.00000000 +00000-0 +33542-4 0 00009
2 57854 53.1615 288.8442 0001146 105.5410 254.5718 15.30187133 00
| Epoch (UTC): | 25 May 2026 02:53:51 |
| Eccentricity: | 0.0001146 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 288.8442° |
| argument of perigee: | 105.5410° |
| revolutions per day: | 15.30187133 |
| mean anomaly at epoch: | 254.5718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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