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 62900U 26145.46286277 +.00000000 +00000-0 +20374-3 0 00009
2 62900 45.0022 63.2476 0007904 8.9414 351.1604 15.15762358 09
| Epoch (UTC): | 25 May 2026 11:06:31 |
| Eccentricity: | 0.0007904 |
| inclination: | 45.0022° |
| perigee height: | 513 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 63.2476° |
| argument of perigee: | 8.9414° |
| revolutions per day: | 15.15762358 |
| mean anomaly at epoch: | 351.1604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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