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 35868U 26108.64230411 +.00000000 +00000-0 +63441-4 0 00003
2 35868 98.7136 71.3030 0005163 85.7123 274.4646 14.24205264 04
| Epoch (UTC): | 18 April 2026 15:24:55 |
| Eccentricity: | 0.0005163 |
| inclination: | 98.7136° |
| perigee height: | 807 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 71.3030° |
| argument of perigee: | 85.7123° |
| revolutions per day: | 14.24205264 |
| mean anomaly at epoch: | 274.4646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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