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 68169U 26145.35538154 +.00000000 +00000-0 +82299-3 0 00008
2 68169 53.1580 270.4612 0001037 117.1252 242.9858 15.38851440 03
| Epoch (UTC): | 25 May 2026 08:31:44 |
| Eccentricity: | 0.0001037 |
| inclination: | 53.1580° |
| perigee height: | 449 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 270.4612° |
| argument of perigee: | 117.1252° |
| revolutions per day: | 15.38851440 |
| mean anomaly at epoch: | 242.9858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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