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 62960U 26145.23755779 +.00000000 +00000-0 +70436-3 0 00002
2 62960 53.1599 237.1650 0001505 101.9956 258.1213 15.30213533 01
| Epoch (UTC): | 25 May 2026 05:42:04 |
| Eccentricity: | 0.0001505 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 237.1650° |
| argument of perigee: | 101.9956° |
| revolutions per day: | 15.30213533 |
| mean anomaly at epoch: | 258.1213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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