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 62634U 26145.49523762 +.00000000 +00000-0 +24674-3 0 00006
2 62634 97.4022 229.9661 0002686 62.9062 297.2455 15.34406304 03
| Epoch (UTC): | 25 May 2026 11:53:08 |
| Eccentricity: | 0.0002686 |
| inclination: | 97.4022° |
| perigee height: | 461 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 229.9661° |
| argument of perigee: | 62.9062° |
| revolutions per day: | 15.34406304 |
| mean anomaly at epoch: | 297.2455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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