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 00045U 26041.95117487 +.00000000 +00000-0 +95880-4 0 00001
2 00045 66.6952 334.0908 0255778 251.8812 105.4283 14.35867170 08
| Epoch (UTC): | 10 February 2026 22:49:41 |
| Eccentricity: | 0.0255778 |
| inclination: | 66.6952° |
| perigee height: | 589 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 334.0908° |
| argument of perigee: | 251.8812° |
| revolutions per day: | 14.35867170 |
| mean anomaly at epoch: | 105.4283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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