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 60258U 26145.16327918 +.00000000 +00000-0 +47366-4 0 00009
2 60258 53.1606 57.4613 0001283 82.8850 277.2297 15.30194676 03
| Epoch (UTC): | 25 May 2026 03:55:07 |
| Eccentricity: | 0.0001283 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.4613° |
| argument of perigee: | 82.8850° |
| revolutions per day: | 15.30194676 |
| mean anomaly at epoch: | 277.2297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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