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 01430U 26088.22510966 +.00000000 +00000-0 +78547-4 0 00001
2 01430 98.4914 207.9551 0054467 320.0429 39.6757 14.41597509 02
| Epoch (UTC): | 29 March 2026 05:24:09 |
| Eccentricity: | 0.0054467 |
| inclination: | 98.4914° |
| perigee height: | 714 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 207.9551° |
| argument of perigee: | 320.0429° |
| revolutions per day: | 14.41597509 |
| mean anomaly at epoch: | 39.6757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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