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 68118U 26145.34881066 +.00000000 +00000-0 +72984-3 0 00004
2 68118 97.2843 106.0116 0001016 98.6233 261.5125 15.33459063 04
| Epoch (UTC): | 25 May 2026 08:22:17 |
| Eccentricity: | 0.0001016 |
| inclination: | 97.2843° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 106.0116° |
| argument of perigee: | 98.6233° |
| revolutions per day: | 15.33459063 |
| mean anomaly at epoch: | 261.5125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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