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 00005U 26048.80207080 +.00000000 +00000-0 +12565-3 0 00005
2 00005 34.2558 322.7675 1838592 320.1489 27.7311 10.85949499 08
| Epoch (UTC): | 17 February 2026 19:14:58 |
| Eccentricity: | 0.1838592 |
| inclination: | 34.2558° |
| perigee height: | 652 km |
| apogee height: | 3819 km |
| right ascension of ascending node: | 322.7675° |
| argument of perigee: | 320.1489° |
| revolutions per day: | 10.85949499 |
| mean anomaly at epoch: | 27.7311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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