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 26071.97946404 +.00000000 +00000-0 +80178-4 0 00004
2 21263 98.6157 61.9294 0012786 313.0641 46.9468 14.26718906 06
| Epoch (UTC): | 12 March 2026 23:30:25 |
| Eccentricity: | 0.0012786 |
| inclination: | 98.6157° |
| perigee height: | 794 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 61.9294° |
| argument of perigee: | 313.0641° |
| revolutions per day: | 14.26718906 |
| mean anomaly at epoch: | 46.9468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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