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 26053.72272432 +.00000000 +00000-0 +71917-4 0 00006
2 00045 66.6936 302.9575 0255298 243.4949 113.9770 14.35875576 03
| Epoch (UTC): | 22 February 2026 17:20:43 |
| Eccentricity: | 0.0255298 |
| inclination: | 66.6936° |
| perigee height: | 590 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 302.9575° |
| argument of perigee: | 243.4949° |
| revolutions per day: | 14.35875576 |
| mean anomaly at epoch: | 113.9770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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