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 54251U 26145.63080895 +.00000000 +00000-0 +58241-3 0 00000
2 54251 97.6169 289.2715 0004087 86.8967 273.2758 15.61879234 04
| Epoch (UTC): | 25 May 2026 15:08:21 |
| Eccentricity: | 0.0004087 |
| inclination: | 97.6169° |
| perigee height: | 379 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 289.2715° |
| argument of perigee: | 86.8967° |
| revolutions per day: | 15.61879234 |
| mean anomaly at epoch: | 273.2758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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