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 68194U 26145.64256795 +.00000000 +00000-0 +57996-3 0 00002
2 68194 53.1587 268.6917 0000798 58.0390 302.0690 15.34396566 05
| Epoch (UTC): | 25 May 2026 15:25:17 |
| Eccentricity: | 0.0000798 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 268.6917° |
| argument of perigee: | 58.0390° |
| revolutions per day: | 15.34396566 |
| mean anomaly at epoch: | 302.0690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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