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 67888U 26145.32513168 +.00000000 +00000-0 +42209-3 0 00007
2 67888 97.2849 78.8643 0001653 90.6770 269.4662 15.33444079 03
| Epoch (UTC): | 25 May 2026 07:48:11 |
| Eccentricity: | 0.0001653 |
| inclination: | 97.2849° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 78.8643° |
| argument of perigee: | 90.6770° |
| revolutions per day: | 15.33444079 |
| mean anomaly at epoch: | 269.4662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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