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 26159.02338422 +.00000000 +00000-0 +81066-4 0 00001
2 27421 97.9850 198.2918 0128442 305.3331 53.5914 14.54745849 01
| Epoch (UTC): | 08 June 2026 00:33:40 |
| Eccentricity: | 0.0128442 |
| inclination: | 97.9850° |
| perigee height: | 619 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 198.2918° |
| argument of perigee: | 305.3331° |
| revolutions per day: | 14.54745849 |
| mean anomaly at epoch: | 53.5914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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