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 54133U 26145.39150382 +.00000000 +00000-0 +35722-3 0 00000
2 54133 87.9179 278.9742 0002005 124.4582 235.6741 13.20772599 04
| Epoch (UTC): | 25 May 2026 09:23:45 |
| Eccentricity: | 0.0002005 |
| inclination: | 87.9179° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9742° |
| argument of perigee: | 124.4582° |
| revolutions per day: | 13.20772599 |
| mean anomaly at epoch: | 235.6741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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