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 26137.79283330 +.00000000 +00000-0 +36764-4 0 00006
2 00045 66.6930 80.5908 0248946 183.0897 176.8683 14.35947846 00
| Epoch (UTC): | 17 May 2026 19:01:40 |
| Eccentricity: | 0.0248946 |
| inclination: | 66.6930° |
| perigee height: | 594 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 80.5908° |
| argument of perigee: | 183.0897° |
| revolutions per day: | 14.35947846 |
| mean anomaly at epoch: | 176.8683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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