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 68435U 26145.61093215 +.00000000 +00000-0 +14283-3 0 00005
2 68435 97.4532 104.3833 0003801 118.2462 241.9156 15.17613492 03
| Epoch (UTC): | 25 May 2026 14:39:44 |
| Eccentricity: | 0.0003801 |
| inclination: | 97.4532° |
| perigee height: | 510 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 104.3833° |
| argument of perigee: | 118.2462° |
| revolutions per day: | 15.17613492 |
| mean anomaly at epoch: | 241.9156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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