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 42268U 26088.01723410 +.00000000 +00000-0 +26053-2 0 00005
2 42268 98.7351 289.5411 0116102 218.8177 140.4610 14.07095638 01
| Epoch (UTC): | 29 March 2026 00:24:49 |
| Eccentricity: | 0.0116102 |
| inclination: | 98.7351° |
| perigee height: | 785 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 289.5411° |
| argument of perigee: | 218.8177° |
| revolutions per day: | 14.07095638 |
| mean anomaly at epoch: | 140.4610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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