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 43099U 26145.60189192 +.00000000 +00000-0 +38425-3 0 00007
2 43099 97.3131 230.4881 0046168 261.5954 98.0057 15.38433372 02
| Epoch (UTC): | 25 May 2026 14:26:43 |
| Eccentricity: | 0.0046168 |
| inclination: | 97.3131° |
| perigee height: | 419 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 230.4881° |
| argument of perigee: | 261.5954° |
| revolutions per day: | 15.38433372 |
| mean anomaly at epoch: | 98.0057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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