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 37264U 26145.36394383 +.00000000 +00000-0 +00000-0 0 00002
2 37264 0.0680 102.1561 0004769 343.7944 258.0234 1.00270849 09
| Epoch (UTC): | 25 May 2026 08:44:04 |
| Eccentricity: | 0.0004769 |
| inclination: | 0.0680° |
| perigee height: | 35767 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 102.1561° |
| argument of perigee: | 343.7944° |
| revolutions per day: | 1.00270849 |
| mean anomaly at epoch: | 258.0234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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