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 26038.14831703 +.00000000 +00000-0 -14272-4 0 00006
2 44909 82.5173 66.1194 0218675 88.4565 274.1571 12.79746880 05
| Epoch (UTC): | 07 February 2026 03:33:34 |
| Eccentricity: | 0.0218675 |
| inclination: | 82.5173° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 66.1194° |
| argument of perigee: | 88.4565° |
| revolutions per day: | 12.79746880 |
| mean anomaly at epoch: | 274.1571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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