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 42354U 26082.99956282 +.00000000 +00000-0 +92781-3 0 00009
2 42354 99.1429 189.0323 0023254 190.7905 169.2773 14.17328696 09
| Epoch (UTC): | 23 March 2026 23:59:22 |
| Eccentricity: | 0.0023254 |
| inclination: | 99.1429° |
| perigee height: | 818 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 189.0323° |
| argument of perigee: | 190.7905° |
| revolutions per day: | 14.17328696 |
| mean anomaly at epoch: | 169.2773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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