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 68259U 26145.41072785 +.00000000 +00000-0 +92227-3 0 00000
2 68259 53.1596 298.0122 0001741 94.3261 265.7944 15.42192486 02
| Epoch (UTC): | 25 May 2026 09:51:26 |
| Eccentricity: | 0.0001741 |
| inclination: | 53.1596° |
| perigee height: | 438 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 298.0122° |
| argument of perigee: | 94.3261° |
| revolutions per day: | 15.42192486 |
| mean anomaly at epoch: | 265.7944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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