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 44316U 26145.56380630 +.00000000 +00000-0 +34961-3 0 00006
2 44316 44.9736 184.3829 0007621 123.7337 236.4272 15.26683825 02
| Epoch (UTC): | 25 May 2026 13:31:52 |
| Eccentricity: | 0.0007621 |
| inclination: | 44.9736° |
| perigee height: | 481 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 184.3829° |
| argument of perigee: | 123.7337° |
| revolutions per day: | 15.26683825 |
| mean anomaly at epoch: | 236.4272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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