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 68547U 26145.33020836 +.00000000 +00000-0 +50346-3 0 00007
2 68547 53.1617 6.2511 0000995 91.9109 268.2008 15.34410667 05
| Epoch (UTC): | 25 May 2026 07:55:30 |
| Eccentricity: | 0.0000995 |
| inclination: | 53.1617° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 6.2511° |
| argument of perigee: | 91.9109° |
| revolutions per day: | 15.34410667 |
| mean anomaly at epoch: | 268.2008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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