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 44882U 26088.25357082 +.00000000 +00000-0 +76269-3 0 00008
2 44882 97.7909 182.3598 0012375 295.1687 64.8255 15.04168565 02
| Epoch (UTC): | 29 March 2026 06:05:08 |
| Eccentricity: | 0.0012375 |
| inclination: | 97.7909° |
| perigee height: | 545 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 182.3598° |
| argument of perigee: | 295.1687° |
| revolutions per day: | 15.04168565 |
| mean anomaly at epoch: | 64.8255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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