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 68018U 26145.39187877 +.00000000 +00000-0 +56455-3 0 00002
2 68018 97.2848 94.3427 0001808 107.6621 252.4819 15.33449027 01
| Epoch (UTC): | 25 May 2026 09:24:18 |
| Eccentricity: | 0.0001808 |
| inclination: | 97.2848° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.3427° |
| argument of perigee: | 107.6621° |
| revolutions per day: | 15.33449027 |
| mean anomaly at epoch: | 252.4819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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