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 27646U 26074.30268829 +.00000000 +00000-0 +15940-3 0 00007
2 27646 49.5192 264.4357 5410395 127.9989 11.4583 4.61718257 03
| Epoch (UTC): | 15 March 2026 07:15:52 |
| Eccentricity: | 0.5410395 |
| inclination: | 49.5192° |
| perigee height: | 614 km |
| apogee height: | 17098 km |
| right ascension of ascending node: | 264.4357° |
| argument of perigee: | 127.9989° |
| revolutions per day: | 4.61718257 |
| mean anomaly at epoch: | 11.4583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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