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 26159.03624103 +.00000000 +00000-0 +97232-4 0 00001
2 00045 66.6943 24.4056 0246865 167.5362 193.2001 14.35960001 02
| Epoch (UTC): | 08 June 2026 00:52:11 |
| Eccentricity: | 0.0246865 |
| inclination: | 66.6943° |
| perigee height: | 595 km |
| apogee height: | 948 km |
| right ascension of ascending node: | 24.4056° |
| argument of perigee: | 167.5362° |
| revolutions per day: | 14.35960001 |
| mean anomaly at epoch: | 193.2001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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