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 08027U 26100.16936375 +.00000000 +00000-0 +36992-4 0 00002
2 08027 81.2994 194.4096 0057271 202.4859 157.3800 14.07769407 06
| Epoch (UTC): | 10 April 2026 04:03:53 |
| Eccentricity: | 0.0057271 |
| inclination: | 81.2994° |
| perigee height: | 826 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 194.4096° |
| argument of perigee: | 202.4859° |
| revolutions per day: | 14.07769407 |
| mean anomaly at epoch: | 157.3800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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