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 26046.13042969 +.00000000 +00000-0 +78001-4 0 00004
2 00045 66.6948 323.0379 0255596 248.9034 108.4571 14.35870412 00
| Epoch (UTC): | 15 February 2026 03:07:49 |
| Eccentricity: | 0.0255596 |
| inclination: | 66.6948° |
| perigee height: | 589 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 323.0379° |
| argument of perigee: | 248.9034° |
| revolutions per day: | 14.35870412 |
| mean anomaly at epoch: | 108.4571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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