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 37206U 26111.84496455 +.00000000 +00000-0 +11615-2 0 00003
2 37206 2.3768 71.8441 6903848 13.2641 358.0851 2.78231401 04
| Epoch (UTC): | 21 April 2026 20:16:44 |
| Eccentricity: | 0.6903848 |
| inclination: | 2.3768° |
| perigee height: | 233 km |
| apogee height: | 29717 km |
| right ascension of ascending node: | 71.8441° |
| argument of perigee: | 13.2641° |
| revolutions per day: | 2.78231401 |
| mean anomaly at epoch: | 358.0851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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