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 62496U 26145.18080131 +.00000000 +00000-0 +71373-3 0 00004
2 62496 43.0003 216.6689 0001335 256.4301 103.6402 15.27602031 03
| Epoch (UTC): | 25 May 2026 04:20:21 |
| Eccentricity: | 0.0001335 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 216.6689° |
| argument of perigee: | 256.4301° |
| revolutions per day: | 15.27602031 |
| mean anomaly at epoch: | 103.6402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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