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 49745U 26145.46303924 +.00000000 +00000-0 -54783-5 0 00004
2 49745 53.2120 164.4429 0001273 54.8795 305.2316 15.08839157 02
| Epoch (UTC): | 25 May 2026 11:06:46 |
| Eccentricity: | 0.0001273 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 164.4429° |
| argument of perigee: | 54.8795° |
| revolutions per day: | 15.08839157 |
| mean anomaly at epoch: | 305.2316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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