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 44499U 26145.32907191 +.00000000 +00000-0 +53406-3 0 00004
2 44499 45.0080 8.0661 0005147 202.5235 157.5436 15.61941653 08
| Epoch (UTC): | 25 May 2026 07:53:51 |
| Eccentricity: | 0.0005147 |
| inclination: | 45.0080° |
| perigee height: | 379 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 8.0661° |
| argument of perigee: | 202.5235° |
| revolutions per day: | 15.61941653 |
| mean anomaly at epoch: | 157.5436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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