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 60102U 26145.43393110 +.00000000 +00000-0 -18106-4 0 00005
2 60102 53.1614 40.8470 0001463 91.6826 268.4342 15.30183059 04
| Epoch (UTC): | 25 May 2026 10:24:51 |
| Eccentricity: | 0.0001463 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.8470° |
| argument of perigee: | 91.6826° |
| revolutions per day: | 15.30183059 |
| mean anomaly at epoch: | 268.4342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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