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 21808U 26158.76289355 +.00000000 +00000-0 +38964-3 0 00002
2 21808 63.2966 178.2640 0884437 74.3046 295.3682 13.59626998 02
| Epoch (UTC): | 07 June 2026 18:18:34 |
| Eccentricity: | 0.0884437 |
| inclination: | 63.2966° |
| perigee height: | 381 km |
| apogee height: | 1693 km |
| right ascension of ascending node: | 178.2640° |
| argument of perigee: | 74.3046° |
| revolutions per day: | 13.59626998 |
| mean anomaly at epoch: | 295.3682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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