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 37606U 26145.60123441 +.00000000 +00000-0 +00000-0 0 00004
2 37606 0.0364 94.2927 0001972 340.4293 112.9215 1.00271437 00
| Epoch (UTC): | 25 May 2026 14:25:46 |
| Eccentricity: | 0.0001972 |
| inclination: | 0.0364° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 94.2927° |
| argument of perigee: | 340.4293° |
| revolutions per day: | 1.00271437 |
| mean anomaly at epoch: | 112.9215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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