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 26042.17381083 +.00000000 +00000-0 +79555-4 0 00007
2 21263 98.6117 32.5951 0014393 40.3049 319.9196 14.26708149 03
| Epoch (UTC): | 11 February 2026 04:10:17 |
| Eccentricity: | 0.0014393 |
| inclination: | 98.6117° |
| perigee height: | 792 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 32.5951° |
| argument of perigee: | 40.3049° |
| revolutions per day: | 14.26708149 |
| mean anomaly at epoch: | 319.9196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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