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 68163U 26145.30707420 +.00000000 +00000-0 +60465-3 0 00002
2 68163 97.2862 166.8811 0000412 243.5753 116.5447 15.33446450 00
| Epoch (UTC): | 25 May 2026 07:22:11 |
| Eccentricity: | 0.0000412 |
| inclination: | 97.2862° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 166.8811° |
| argument of perigee: | 243.5753° |
| revolutions per day: | 15.33446450 |
| mean anomaly at epoch: | 116.5447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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