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 62829U 26145.55947389 +.00000000 +00000-0 +11529-2 0 00008
2 62829 43.0003 202.3450 0001388 256.7345 103.3368 15.70859731 07
| Epoch (UTC): | 25 May 2026 13:25:38 |
| Eccentricity: | 0.0001388 |
| inclination: | 43.0003° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 202.3450° |
| argument of perigee: | 256.7345° |
| revolutions per day: | 15.70859731 |
| mean anomaly at epoch: | 103.3368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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