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 68164U 26145.48380650 +.00000000 +00000-0 +72965-3 0 00002
2 68164 97.2857 167.0972 0000382 343.5223 16.6007 15.33455356 02
| Epoch (UTC): | 25 May 2026 11:36:40 |
| Eccentricity: | 0.0000382 |
| inclination: | 97.2857° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 167.0972° |
| argument of perigee: | 343.5223° |
| revolutions per day: | 15.33455356 |
| mean anomaly at epoch: | 16.6007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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