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 44804U 26145.63213279 +.00000000 +00000-0 +32456-3 0 00007
2 44804 97.4317 207.8597 0011506 224.7550 135.2757 15.19270436 07
| Epoch (UTC): | 25 May 2026 15:10:16 |
| Eccentricity: | 0.0011506 |
| inclination: | 97.4317° |
| perigee height: | 500 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 207.8597° |
| argument of perigee: | 224.7550° |
| revolutions per day: | 15.19270436 |
| mean anomaly at epoch: | 135.2757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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