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 45706U 26145.58335647 +.00000000 +00000-0 +91207-3 0 00006
2 45706 53.0328 320.1643 0003685 278.7919 163.4202 15.83702656 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0003685 |
| inclination: | 53.0328° |
| perigee height: | 318 km |
| apogee height: | 322 km |
| right ascension of ascending node: | 320.1643° |
| argument of perigee: | 278.7919° |
| revolutions per day: | 15.83702656 |
| mean anomaly at epoch: | 163.4202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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