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 45744U 26145.41727994 +.00000000 +00000-0 +54366-3 0 00005
2 45744 53.0341 191.7312 0002162 96.4557 263.6692 15.38494608 05
| Epoch (UTC): | 25 May 2026 10:00:52 |
| Eccentricity: | 0.0002162 |
| inclination: | 53.0341° |
| perigee height: | 449 km |
| apogee height: | 452 km |
| right ascension of ascending node: | 191.7312° |
| argument of perigee: | 96.4557° |
| revolutions per day: | 15.38494608 |
| mean anomaly at epoch: | 263.6692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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