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 26069.42515611 +.00000000 +00000-0 +65263-4 0 00006
2 21088 82.9466 169.4993 0023037 36.3190 33.8205 13.77494337 03
| Epoch (UTC): | 10 March 2026 10:12:13 |
| Eccentricity: | 0.0023037 |
| inclination: | 82.9466° |
| perigee height: | 956 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 169.4993° |
| argument of perigee: | 36.3190° |
| revolutions per day: | 13.77494337 |
| mean anomaly at epoch: | 33.8205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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