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 68440U 26145.38749429 +.00000000 +00000-0 +92966-3 0 00004
2 68440 97.4493 104.1972 0005225 116.2705 243.9067 15.19266070 08
| Epoch (UTC): | 25 May 2026 09:17:59 |
| Eccentricity: | 0.0005225 |
| inclination: | 97.4493° |
| perigee height: | 504 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 104.1972° |
| argument of perigee: | 116.2705° |
| revolutions per day: | 15.19266070 |
| mean anomaly at epoch: | 243.9067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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