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 60280U 26145.04944531 +.00000000 +00000-0 +68256-4 0 00008
2 60280 53.1590 57.5892 0001221 92.5187 267.5953 15.30194976 07
| Epoch (UTC): | 25 May 2026 01:11:12 |
| Eccentricity: | 0.0001221 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.5892° |
| argument of perigee: | 92.5187° |
| revolutions per day: | 15.30194976 |
| mean anomaly at epoch: | 267.5953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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