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 62733U 26145.57094991 +.00000000 +00000-0 +17442-3 0 00007
2 62733 97.6550 314.9144 0010103 95.5575 264.6807 15.10909857 00
| Epoch (UTC): | 25 May 2026 13:42:10 |
| Eccentricity: | 0.0010103 |
| inclination: | 97.6550° |
| perigee height: | 526 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 314.9144° |
| argument of perigee: | 95.5575° |
| revolutions per day: | 15.10909857 |
| mean anomaly at epoch: | 264.6807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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