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 26071.04387542 +.00000000 +00000-0 +63491-4 0 00008
2 21088 82.9465 168.2958 0022941 31.9006 140.9010 13.77494607 04
| Epoch (UTC): | 12 March 2026 01:03:10 |
| Eccentricity: | 0.0022941 |
| inclination: | 82.9465° |
| perigee height: | 956 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 168.2958° |
| argument of perigee: | 31.9006° |
| revolutions per day: | 13.77494607 |
| mean anomaly at epoch: | 140.9010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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