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 60274U 26145.47858417 +.00000000 +00000-0 +32360-5 0 00003
2 60274 53.1627 55.8721 0001348 95.7567 264.3588 15.31699601 05
| Epoch (UTC): | 25 May 2026 11:29:09 |
| Eccentricity: | 0.0001348 |
| inclination: | 53.1627° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 55.8721° |
| argument of perigee: | 95.7567° |
| revolutions per day: | 15.31699601 |
| mean anomaly at epoch: | 264.3588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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