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 62731U 26100.18718583 +.00000000 +00000-0 +22590-3 0 00003
2 62731 97.6467 269.2846 0012964 242.9447 117.0460 15.10842830 02
| Epoch (UTC): | 10 April 2026 04:29:32 |
| Eccentricity: | 0.0012964 |
| inclination: | 97.6467° |
| perigee height: | 525 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 269.2846° |
| argument of perigee: | 242.9447° |
| revolutions per day: | 15.10842830 |
| mean anomaly at epoch: | 117.0460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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