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 68243U 26145.66635963 +.00000000 +00000-0 +58075-3 0 00006
2 68243 53.1612 292.4085 0000341 170.7926 189.3083 15.34391779 04
| Epoch (UTC): | 25 May 2026 15:59:33 |
| Eccentricity: | 0.0000341 |
| inclination: | 53.1612° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 292.4085° |
| argument of perigee: | 170.7926° |
| revolutions per day: | 15.34391779 |
| mean anomaly at epoch: | 189.3083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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