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 37610U 26087.67503550 +.00000000 +00000-0 +40125-3 0 00009
2 37610 99.1177 346.9265 0151562 69.8103 291.9277 13.78090568 09
| Epoch (UTC): | 28 March 2026 16:12:03 |
| Eccentricity: | 0.0151562 |
| inclination: | 99.1177° |
| perigee height: | 859 km |
| apogee height: | 1082 km |
| right ascension of ascending node: | 346.9265° |
| argument of perigee: | 69.8103° |
| revolutions per day: | 13.78090568 |
| mean anomaly at epoch: | 291.9277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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