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 60054U 26145.23495461 +.00000000 +00000-0 +34464-4 0 00005
2 60054 53.1602 82.6153 0001237 75.5849 284.5289 15.30196344 04
| Epoch (UTC): | 25 May 2026 05:38:20 |
| Eccentricity: | 0.0001237 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 82.6153° |
| argument of perigee: | 75.5849° |
| revolutions per day: | 15.30196344 |
| mean anomaly at epoch: | 284.5289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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