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 26074.81427103 +.00000000 +00000-0 +36750-4 0 00009
2 44909 82.5215 41.7436 0217672 3.0207 357.2151 12.79747585 02
| Epoch (UTC): | 15 March 2026 19:32:33 |
| Eccentricity: | 0.0217672 |
| inclination: | 82.5215° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 41.7436° |
| argument of perigee: | 3.0207° |
| revolutions per day: | 12.79747585 |
| mean anomaly at epoch: | 357.2151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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