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 44909U 26074.26702236 +.00000000 +00000-0 +27334-4 0 00009
2 44909 82.5213 42.1072 0217694 4.2999 355.9905 12.79747544 03
| Epoch (UTC): | 15 March 2026 06:24:30 |
| Eccentricity: | 0.0217694 |
| inclination: | 82.5213° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 42.1072° |
| argument of perigee: | 4.2999° |
| revolutions per day: | 12.79747544 |
| mean anomaly at epoch: | 355.9905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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