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 54136U 26145.40060679 +.00000000 +00000-0 +27745-3 0 00000
2 54136 87.9151 309.5174 0001611 91.9256 268.2061 13.19725387 03
| Epoch (UTC): | 25 May 2026 09:36:52 |
| Eccentricity: | 0.0001611 |
| inclination: | 87.9151° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5174° |
| argument of perigee: | 91.9256° |
| revolutions per day: | 13.19725387 |
| mean anomaly at epoch: | 268.2061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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