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 21088U 26137.72399508 +.00000000 +00000-0 -52713-4 0 00007
2 21088 82.9398 118.6970 0021868 198.3350 334.6042 13.77504800 03
| Epoch (UTC): | 17 May 2026 17:22:33 |
| Eccentricity: | 0.0021868 |
| inclination: | 82.9398° |
| perigee height: | 957 km |
| apogee height: | 989 km |
| right ascension of ascending node: | 118.6970° |
| argument of perigee: | 198.3350° |
| revolutions per day: | 13.77504800 |
| mean anomaly at epoch: | 334.6042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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