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 62624U 26145.22268878 +.00000000 +00000-0 +41144-3 0 00001
2 62624 97.3945 226.6789 0003709 66.3341 293.8288 15.28756826 01
| Epoch (UTC): | 25 May 2026 05:20:40 |
| Eccentricity: | 0.0003709 |
| inclination: | 97.3945° |
| perigee height: | 477 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 226.6789° |
| argument of perigee: | 66.3341° |
| revolutions per day: | 15.28756826 |
| mean anomaly at epoch: | 293.8288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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