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 45098U 26145.33937914 +.00000000 +00000-0 +11717-2 0 00005
2 45098 53.0523 258.2801 0003846 6.0326 354.0712 15.13627667 06
| Epoch (UTC): | 25 May 2026 08:08:42 |
| Eccentricity: | 0.0003846 |
| inclination: | 53.0523° |
| perigee height: | 522 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 258.2801° |
| argument of perigee: | 6.0326° |
| revolutions per day: | 15.13627667 |
| mean anomaly at epoch: | 354.0712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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