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 68723U 26145.41333720 +.00000000 +00000-0 +62506-3 0 00002
2 68723 53.1604 38.1418 0000975 102.7639 257.3479 15.49337926 07
| Epoch (UTC): | 25 May 2026 09:55:12 |
| Eccentricity: | 0.0000975 |
| inclination: | 53.1604° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 38.1418° |
| argument of perigee: | 102.7639° |
| revolutions per day: | 15.49337926 |
| mean anomaly at epoch: | 257.3479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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