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 68196U 26145.61703677 +.00000000 +00000-0 +10683-3 0 00009
2 68196 141.9854 218.5928 0001081 289.9156 70.1448 13.83263346 02
| Epoch (UTC): | 25 May 2026 14:48:31 |
| Eccentricity: | 0.0001081 |
| inclination: | 141.9854° |
| perigee height: | 952 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 218.5928° |
| argument of perigee: | 289.9156° |
| revolutions per day: | 13.83263346 |
| mean anomaly at epoch: | 70.1448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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