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 21228U 26158.38332144 +.00000000 +00000-0 +79938-4 0 00008
2 21228 23.9905 183.8894 1133121 165.5352 198.0502 12.55631211 07
| Epoch (UTC): | 07 June 2026 09:11:58 |
| Eccentricity: | 0.1133121 |
| inclination: | 23.9905° |
| perigee height: | 555 km |
| apogee height: | 2327 km |
| right ascension of ascending node: | 183.8894° |
| argument of perigee: | 165.5352° |
| revolutions per day: | 12.55631211 |
| mean anomaly at epoch: | 198.0502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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