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 68232U 26145.41844022 +.00000000 +00000-0 +80401-3 0 00003
2 68232 53.1599 293.7151 0000710 68.0043 292.1035 15.34410392 06
| Epoch (UTC): | 25 May 2026 10:02:33 |
| Eccentricity: | 0.0000710 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 293.7151° |
| argument of perigee: | 68.0043° |
| revolutions per day: | 15.34410392 |
| mean anomaly at epoch: | 292.1035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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