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 61768U 26145.60900985 +.00000000 +00000-0 +42611-3 0 00003
2 61768 97.3001 20.1662 0006071 31.3734 328.7878 15.48565507 01
| Epoch (UTC): | 25 May 2026 14:36:58 |
| Eccentricity: | 0.0006071 |
| inclination: | 97.3001° |
| perigee height: | 417 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 20.1662° |
| argument of perigee: | 31.3734° |
| revolutions per day: | 15.48565507 |
| mean anomaly at epoch: | 328.7878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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