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 27421U 26066.09707520 +.00000000 +00000-0 +12358-3 0 00001
2 27421 97.9992 109.4256 0128746 233.6378 125.2884 14.54657432 01
| Epoch (UTC): | 07 March 2026 02:19:47 |
| Eccentricity: | 0.0128746 |
| inclination: | 97.9992° |
| perigee height: | 619 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 109.4256° |
| argument of perigee: | 233.6378° |
| revolutions per day: | 14.54657432 |
| mean anomaly at epoch: | 125.2884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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