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 44885U 26112.19013388 +.00000000 +00000-0 +57031-3 0 00006
2 44885 97.7904 206.0467 0010303 254.8541 105.1545 15.03269964 04
| Epoch (UTC): | 22 April 2026 04:33:47 |
| Eccentricity: | 0.0010303 |
| inclination: | 97.7904° |
| perigee height: | 550 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 206.0467° |
| argument of perigee: | 254.8541° |
| revolutions per day: | 15.03269964 |
| mean anomaly at epoch: | 105.1545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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