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 37750U 26131.76978326 +.00000000 +00000-0 -15822-3 0 00008
2 37750 45.2467 67.7918 6353282 307.0653 10.2947 3.31079591 04
| Epoch (UTC): | 11 May 2026 18:28:29 |
| Eccentricity: | 0.6353282 |
| inclination: | 45.2467° |
| perigee height: | 556 km |
| apogee height: | 24719 km |
| right ascension of ascending node: | 67.7918° |
| argument of perigee: | 307.0653° |
| revolutions per day: | 3.31079591 |
| mean anomaly at epoch: | 10.2947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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