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 21048U 26088.12226684 +.00000000 +00000-0 +67447-4 0 00005
2 21048 18.4508 211.6749 1187790 135.0466 235.2392 11.85460967 04
| Epoch (UTC): | 29 March 2026 02:56:03 |
| Eccentricity: | 0.1187790 |
| inclination: | 18.4508° |
| perigee height: | 782 km |
| apogee height: | 2712 km |
| right ascension of ascending node: | 211.6749° |
| argument of perigee: | 135.0466° |
| revolutions per day: | 11.85460967 |
| mean anomaly at epoch: | 235.2392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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