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 68204U 26145.14869175 +.00000000 +00000-0 +23754-3 0 00006
2 68204 97.5334 220.3629 0010912 36.4771 323.7201 15.11366324 08
| Epoch (UTC): | 25 May 2026 03:34:06 |
| Eccentricity: | 0.0010912 |
| inclination: | 97.5334° |
| perigee height: | 524 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 220.3629° |
| argument of perigee: | 36.4771° |
| revolutions per day: | 15.11366324 |
| mean anomaly at epoch: | 323.7201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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