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 62768U 26144.94799139 +.00000000 +00000-0 +44125-3 0 00009
2 62768 53.1594 327.7474 0000703 95.0811 265.0271 15.34405995 04
| Epoch (UTC): | 24 May 2026 22:45:06 |
| Eccentricity: | 0.0000703 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 327.7474° |
| argument of perigee: | 95.0811° |
| revolutions per day: | 15.34405995 |
| mean anomaly at epoch: | 265.0271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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