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 44850U 26145.03552454 +.00000000 +00000-0 +00000-0 0 00000
2 44850 65.5540 74.5027 0013925 261.2351 98.5977 2.13101726 01
| Epoch (UTC): | 25 May 2026 00:51:09 |
| Eccentricity: | 0.0013925 |
| inclination: | 65.5540° |
| perigee height: | 19094 km |
| apogee height: | 19165 km |
| right ascension of ascending node: | 74.5027° |
| argument of perigee: | 261.2351° |
| revolutions per day: | 2.13101726 |
| mean anomaly at epoch: | 98.5977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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