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 60263U 26145.46458041 +.00000000 +00000-0 +10351-3 0 00003
2 60263 53.1606 55.7865 0001403 85.8530 274.2632 15.31714045 00
| Epoch (UTC): | 25 May 2026 11:08:59 |
| Eccentricity: | 0.0001403 |
| inclination: | 53.1606° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 55.7865° |
| argument of perigee: | 85.8530° |
| revolutions per day: | 15.31714045 |
| mean anomaly at epoch: | 274.2632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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