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 42836U 26067.94817676 +.00000000 +00000-0 +52591-3 0 00000
2 42836 97.4136 233.3001 0005156 85.6250 274.5567 15.07977711 01
| Epoch (UTC): | 08 March 2026 22:45:22 |
| Eccentricity: | 0.0005156 |
| inclination: | 97.4136° |
| perigee height: | 539 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 233.3001° |
| argument of perigee: | 85.6250° |
| revolutions per day: | 15.07977711 |
| mean anomaly at epoch: | 274.5567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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