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 26101.50461794 +.00000000 +00000-0 +91187-4 0 00008
2 00045 66.6934 176.5746 0252303 209.3376 149.3363 14.35931942 06
| Epoch (UTC): | 11 April 2026 12:06:38 |
| Eccentricity: | 0.0252303 |
| inclination: | 66.6934° |
| perigee height: | 592 km |
| apogee height: | 952 km |
| right ascension of ascending node: | 176.5746° |
| argument of perigee: | 209.3376° |
| revolutions per day: | 14.35931942 |
| mean anomaly at epoch: | 149.3363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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