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 67968U 26145.46433178 +.00000000 +00000-0 +68884-3 0 00000
2 67968 97.2846 155.4657 0001195 99.0026 261.1352 15.33439341 05
| Epoch (UTC): | 25 May 2026 11:08:38 |
| Eccentricity: | 0.0001195 |
| inclination: | 97.2846° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.4657° |
| argument of perigee: | 99.0026° |
| revolutions per day: | 15.33439341 |
| mean anomaly at epoch: | 261.1352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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