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 27945U 26053.17905141 +.00000000 +00000-0 +96445-4 0 00006
2 27945 98.3702 219.2940 0011052 344.9771 15.1103 14.67770602 00
| Epoch (UTC): | 22 February 2026 04:17:50 |
| Eccentricity: | 0.0011052 |
| inclination: | 98.3702° |
| perigee height: | 660 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 219.2940° |
| argument of perigee: | 344.9771° |
| revolutions per day: | 14.67770602 |
| mean anomaly at epoch: | 15.1103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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