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 60299U 26144.95606441 +.00000000 +00000-0 +36483-4 0 00009
2 60299 53.1627 29.7352 0001307 84.0885 276.0264 15.30192440 00
| Epoch (UTC): | 24 May 2026 22:56:43 |
| Eccentricity: | 0.0001307 |
| inclination: | 53.1627° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 29.7352° |
| argument of perigee: | 84.0885° |
| revolutions per day: | 15.30192440 |
| mean anomaly at epoch: | 276.0264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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