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 62644U 26144.80746619 +.00000000 +00000-0 +12519-2 0 00003
2 62644 97.4018 230.9752 0002387 63.8375 296.3118 15.44397173 07
| Epoch (UTC): | 24 May 2026 19:22:45 |
| Eccentricity: | 0.0002387 |
| inclination: | 97.4018° |
| perigee height: | 432 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 230.9752° |
| argument of perigee: | 63.8375° |
| revolutions per day: | 15.44397173 |
| mean anomaly at epoch: | 296.3118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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