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 60099U 26144.98927105 +.00000000 +00000-0 +32213-4 0 00000
2 60099 53.1614 42.3372 0001295 83.0683 277.0465 15.30191414 02
| Epoch (UTC): | 24 May 2026 23:44:33 |
| Eccentricity: | 0.0001295 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 42.3372° |
| argument of perigee: | 83.0683° |
| revolutions per day: | 15.30191414 |
| mean anomaly at epoch: | 277.0465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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