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 21140U 26150.28908522 +.00000000 +00000-0 +00000-0 0 00001
2 21140 14.6609 350.1283 0009674 269.5466 91.4643 0.98453137 09
| Epoch (UTC): | 30 May 2026 06:56:16 |
| Eccentricity: | 0.0009674 |
| inclination: | 14.6609° |
| perigee height: | 36263 km |
| apogee height: | 36346 km |
| right ascension of ascending node: | 350.1283° |
| argument of perigee: | 269.5466° |
| revolutions per day: | 0.98453137 |
| mean anomaly at epoch: | 91.4643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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