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 43277U 26145.62076562 +.00000000 +00000-0 -18658-3 0 00000
2 43277 63.3939 148.7126 0273554 7.0350 353.4394 13.45440128 01
| Epoch (UTC): | 25 May 2026 14:53:54 |
| Eccentricity: | 0.0273554 |
| inclination: | 63.3939° |
| perigee height: | 885 km |
| apogee height: | 1293 km |
| right ascension of ascending node: | 148.7126° |
| argument of perigee: | 7.0350° |
| revolutions per day: | 13.45440128 |
| mean anomaly at epoch: | 353.4394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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