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 54137U 26145.42587044 +.00000000 +00000-0 +71052-4 0 00004
2 54137 87.9162 309.5012 0001992 92.1265 268.0096 13.19722151 04
| Epoch (UTC): | 25 May 2026 10:13:15 |
| Eccentricity: | 0.0001992 |
| inclination: | 87.9162° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5012° |
| argument of perigee: | 92.1265° |
| revolutions per day: | 13.19722151 |
| mean anomaly at epoch: | 268.0096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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