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 62639U 26145.15628713 +.00000000 +00000-0 +37601-3 0 00000
2 62639 97.4026 227.2784 0003412 52.8236 307.3315 15.28814728 02
| Epoch (UTC): | 25 May 2026 03:45:03 |
| Eccentricity: | 0.0003412 |
| inclination: | 97.4026° |
| perigee height: | 477 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 227.2784° |
| argument of perigee: | 52.8236° |
| revolutions per day: | 15.28814728 |
| mean anomaly at epoch: | 307.3315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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