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 21263U 26088.10950729 +.00000000 +00000-0 +75808-4 0 00006
2 21263 98.6173 77.8112 0012483 261.9527 98.0237 14.26723722 01
| Epoch (UTC): | 29 March 2026 02:37:41 |
| Eccentricity: | 0.0012483 |
| inclination: | 98.6173° |
| perigee height: | 794 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 77.8112° |
| argument of perigee: | 261.9527° |
| revolutions per day: | 14.26723722 |
| mean anomaly at epoch: | 98.0237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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