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 67881U 26145.37951120 +.00000000 +00000-0 +68464-3 0 00000
2 67881 97.2852 78.9436 0001635 93.2475 266.8955 15.33450777 00
| Epoch (UTC): | 25 May 2026 09:06:29 |
| Eccentricity: | 0.0001635 |
| inclination: | 97.2852° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 78.9436° |
| argument of perigee: | 93.2475° |
| revolutions per day: | 15.33450777 |
| mean anomaly at epoch: | 266.8955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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