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 26039.23465435 +.00000000 +00000-0 +12355-3 0 00003
2 00045 66.6950 341.2749 0255912 253.8061 103.4743 14.35864781 01
| Epoch (UTC): | 08 February 2026 05:37:54 |
| Eccentricity: | 0.0255912 |
| inclination: | 66.6950° |
| perigee height: | 589 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 341.2749° |
| argument of perigee: | 253.8061° |
| revolutions per day: | 14.35864781 |
| mean anomaly at epoch: | 103.4743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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