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 44520U 26067.02255766 +.00000000 +00000-0 +25072-3 0 00001
2 44520 97.7823 80.8866 0009717 328.4981 31.5657 14.96380361 06
| Epoch (UTC): | 08 March 2026 00:32:28 |
| Eccentricity: | 0.0009717 |
| inclination: | 97.7823° |
| perigee height: | 571 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 80.8866° |
| argument of perigee: | 328.4981° |
| revolutions per day: | 14.96380361 |
| mean anomaly at epoch: | 31.5657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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