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 26064.19494985 +.00000000 +00000-0 +85239-4 0 00005
2 21263 98.6148 54.2663 0013172 336.8993 23.1594 14.26715785 03
| Epoch (UTC): | 05 March 2026 04:40:43 |
| Eccentricity: | 0.0013172 |
| inclination: | 98.6148° |
| perigee height: | 793 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 54.2663° |
| argument of perigee: | 336.8993° |
| revolutions per day: | 14.26715785 |
| mean anomaly at epoch: | 23.1594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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