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 26073.27150141 +.00000000 +00000-0 +47841-4 0 00009
2 21088 82.9464 166.6399 0022811 25.8665 27.4491 13.77494874 01
| Epoch (UTC): | 14 March 2026 06:30:57 |
| Eccentricity: | 0.0022811 |
| inclination: | 82.9464° |
| perigee height: | 956 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 166.6399° |
| argument of perigee: | 25.8665° |
| revolutions per day: | 13.77494874 |
| mean anomaly at epoch: | 27.4491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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