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 37845U 26067.33785161 +.00000000 +00000-0 +78759-3 0 00004
2 37845 49.7076 47.1877 4512995 148.3157 249.3377 6.45023464 09
| Epoch (UTC): | 08 March 2026 08:06:30 |
| Eccentricity: | 0.4512995 |
| inclination: | 49.7076° |
| perigee height: | 311 km |
| apogee height: | 11314 km |
| right ascension of ascending node: | 47.1877° |
| argument of perigee: | 148.3157° |
| revolutions per day: | 6.45023464 |
| mean anomaly at epoch: | 249.3377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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