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 21305U 26088.18219968 +.00000000 +00000-0 +11148-3 0 00000
2 21305 82.5615 118.6791 0037556 203.6013 219.9120 12.54825544 08
| Epoch (UTC): | 29 March 2026 04:22:22 |
| Eccentricity: | 0.0037556 |
| inclination: | 82.5615° |
| perigee height: | 1415 km |
| apogee height: | 1474 km |
| right ascension of ascending node: | 118.6791° |
| argument of perigee: | 203.6013° |
| revolutions per day: | 12.54825544 |
| mean anomaly at epoch: | 219.9120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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