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 68339U 26144.99392971 +.00000000 +00000-0 +65495-3 0 00000
2 68339 53.1578 353.4437 0000927 79.3656 280.7450 15.30215503 04
| Epoch (UTC): | 24 May 2026 23:51:15 |
| Eccentricity: | 0.0000927 |
| inclination: | 53.1578° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 353.4437° |
| argument of perigee: | 79.3656° |
| revolutions per day: | 15.30215503 |
| mean anomaly at epoch: | 280.7450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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