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 67788U 26145.48584551 +.00000000 +00000-0 +97247-2 0 00008
2 67788 51.8998 216.0329 0001410 112.6596 247.4515 14.79755923 07
| Epoch (UTC): | 25 May 2026 11:39:37 |
| Eccentricity: | 0.0001410 |
| inclination: | 51.8998° |
| perigee height: | 629 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 216.0329° |
| argument of perigee: | 112.6596° |
| revolutions per day: | 14.79755923 |
| mean anomaly at epoch: | 247.4515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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