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 68840U 26145.51170987 +.00000000 +00000-0 +10640-2 0 00008
2 68840 97.2861 160.1275 0000313 122.1189 238.0093 15.49220259 08
| Epoch (UTC): | 25 May 2026 12:16:51 |
| Eccentricity: | 0.0000313 |
| inclination: | 97.2861° |
| perigee height: | 419 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 160.1275° |
| argument of perigee: | 122.1189° |
| revolutions per day: | 15.49220259 |
| mean anomaly at epoch: | 238.0093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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