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 68360U 26145.17829633 +.00000000 +00000-0 +29628-3 0 00003
2 68360 82.2957 38.1076 0006907 183.3818 176.7406 15.86112360 01
| Epoch (UTC): | 25 May 2026 04:16:44 |
| Eccentricity: | 0.0006907 |
| inclination: | 82.2957° |
| perigee height: | 309 km |
| apogee height: | 318 km |
| right ascension of ascending node: | 38.1076° |
| argument of perigee: | 183.3818° |
| revolutions per day: | 15.86112360 |
| mean anomaly at epoch: | 176.7406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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