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 68162U 26145.01886369 +.00000000 +00000-0 +26938-3 0 00006
2 68162 97.2862 166.6586 0000501 331.5722 28.5494 15.33443038 02
| Epoch (UTC): | 25 May 2026 00:27:09 |
| Eccentricity: | 0.0000501 |
| inclination: | 97.2862° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 166.6586° |
| argument of perigee: | 331.5722° |
| revolutions per day: | 15.33443038 |
| mean anomaly at epoch: | 28.5494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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