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 46025U 26145.62055081 +.00000000 +00000-0 +39776-3 0 00000
2 46025 97.2439 214.9194 0011207 164.5511 195.6078 15.36696318 01
| Epoch (UTC): | 25 May 2026 14:53:35 |
| Eccentricity: | 0.0011207 |
| inclination: | 97.2439° |
| perigee height: | 448 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 214.9194° |
| argument of perigee: | 164.5511° |
| revolutions per day: | 15.36696318 |
| mean anomaly at epoch: | 195.6078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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