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 26066.87308238 +.00000000 +00000-0 +75838-3 0 00003
2 37845 49.7070 47.6774 4513088 147.9028 250.1096 6.45018602 06
| Epoch (UTC): | 07 March 2026 20:57:14 |
| Eccentricity: | 0.4513088 |
| inclination: | 49.7070° |
| perigee height: | 311 km |
| apogee height: | 11314 km |
| right ascension of ascending node: | 47.6774° |
| argument of perigee: | 147.9028° |
| revolutions per day: | 6.45018602 |
| mean anomaly at epoch: | 250.1096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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