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 43279U 26145.63120734 +.00000000 +00000-0 -12707-3 0 00003
2 43279 63.3933 149.9056 0273216 7.7540 352.7581 13.45368671 07
| Epoch (UTC): | 25 May 2026 15:08:56 |
| Eccentricity: | 0.0273216 |
| inclination: | 63.3933° |
| perigee height: | 885 km |
| apogee height: | 1293 km |
| right ascension of ascending node: | 149.9056° |
| argument of perigee: | 7.7540° |
| revolutions per day: | 13.45368671 |
| mean anomaly at epoch: | 352.7581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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