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 68267U 26145.51635806 +.00000000 +00000-0 +67013-3 0 00004
2 68267 53.1580 320.9807 0001144 74.8196 285.2933 15.35424439 09
| Epoch (UTC): | 25 May 2026 12:23:33 |
| Eccentricity: | 0.0001144 |
| inclination: | 53.1580° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 320.9807° |
| argument of perigee: | 74.8196° |
| revolutions per day: | 15.35424439 |
| mean anomaly at epoch: | 285.2933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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