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 60283U 26145.46455145 +.00000000 +00000-0 -72213-4 0 00004
2 60283 53.1620 55.9113 0001202 87.3288 272.7850 15.30199854 09
| Epoch (UTC): | 25 May 2026 11:08:57 |
| Eccentricity: | 0.0001202 |
| inclination: | 53.1620° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 55.9113° |
| argument of perigee: | 87.3288° |
| revolutions per day: | 15.30199854 |
| mean anomaly at epoch: | 272.7850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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