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 26074.67557851 +.00000000 +00000-0 +52614-4 0 00007
2 21088 82.9462 165.5960 0022723 22.0556 150.1194 13.77495081 06
| Epoch (UTC): | 15 March 2026 16:12:49 |
| Eccentricity: | 0.0022723 |
| inclination: | 82.9462° |
| perigee height: | 956 km |
| apogee height: | 989 km |
| right ascension of ascending node: | 165.5960° |
| argument of perigee: | 22.0556° |
| revolutions per day: | 13.77495081 |
| mean anomaly at epoch: | 150.1194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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