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 26039.09534559 +.00000000 +00000-0 +11950-3 0 00001
2 00045 66.6950 341.6434 0255923 253.9043 103.3747 14.35864493 02
| Epoch (UTC): | 08 February 2026 02:17:17 |
| Eccentricity: | 0.0255923 |
| inclination: | 66.6950° |
| perigee height: | 589 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 341.6434° |
| argument of perigee: | 253.9043° |
| revolutions per day: | 14.35864493 |
| mean anomaly at epoch: | 103.3747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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