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 68543U 26145.34282356 +.00000000 +00000-0 +51702-3 0 00008
2 68543 53.1609 6.3311 0000776 89.4748 270.6343 15.34423044 01
| Epoch (UTC): | 25 May 2026 08:13:39 |
| Eccentricity: | 0.0000776 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 6.3311° |
| argument of perigee: | 89.4748° |
| revolutions per day: | 15.34423044 |
| mean anomaly at epoch: | 270.6343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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