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 60287U 26145.02150875 +.00000000 +00000-0 +22641-4 0 00001
2 60287 53.1617 58.1217 0001294 87.8917 272.2233 15.31699174 05
| Epoch (UTC): | 25 May 2026 00:30:58 |
| Eccentricity: | 0.0001294 |
| inclination: | 53.1617° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 58.1217° |
| argument of perigee: | 87.8917° |
| revolutions per day: | 15.31699174 |
| mean anomaly at epoch: | 272.2233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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