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 45726U 26145.50672045 +.00000000 +00000-0 +12850-3 0 00003
2 45726 97.7856 338.2445 0007643 242.8215 117.2233 15.05551851 06
| Epoch (UTC): | 25 May 2026 12:09:40 |
| Eccentricity: | 0.0007643 |
| inclination: | 97.7856° |
| perigee height: | 545 km |
| apogee height: | 555 km |
| right ascension of ascending node: | 338.2445° |
| argument of perigee: | 242.8215° |
| revolutions per day: | 15.05551851 |
| mean anomaly at epoch: | 117.2233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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