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 37749U 26145.45829353 +.00000000 +00000-0 +00000-0 0 00000
2 37749 0.0392 258.3676 0000505 220.3262 15.8399 1.00273333 07
| Epoch (UTC): | 25 May 2026 10:59:56 |
| Eccentricity: | 0.0000505 |
| inclination: | 0.0392° |
| perigee height: | 35784 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 258.3676° |
| argument of perigee: | 220.3262° |
| revolutions per day: | 1.00273333 |
| mean anomaly at epoch: | 15.8399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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