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 21088U 26157.08518081 +.00000000 +00000-0 +37465-4 0 00003
2 21088 82.9417 104.2923 0023148 144.2927 226.8552 13.77505097 04
| Epoch (UTC): | 06 June 2026 02:02:39 |
| Eccentricity: | 0.0023148 |
| inclination: | 82.9417° |
| perigee height: | 956 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 104.2923° |
| argument of perigee: | 144.2927° |
| revolutions per day: | 13.77505097 |
| mean anomaly at epoch: | 226.8552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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