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 22116U 26106.40904500 +.00000000 +00000-0 +00000-0 0 00002
2 22116 14.1527 10.7230 0006598 325.7322 216.7682 0.99317418 03
| Epoch (UTC): | 16 April 2026 09:49:01 |
| Eccentricity: | 0.0006598 |
| inclination: | 14.1527° |
| perigee height: | 36028 km |
| apogee height: | 36084 km |
| right ascension of ascending node: | 10.7230° |
| argument of perigee: | 325.7322° |
| revolutions per day: | 0.99317418 |
| mean anomaly at epoch: | 216.7682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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