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 68948U 26145.37141784 +.00000000 +00000-0 +26640-3 0 00002
2 68948 51.8770 178.3288 0016238 60.8650 299.3956 15.28983199 05
| Epoch (UTC): | 25 May 2026 08:54:50 |
| Eccentricity: | 0.0016238 |
| inclination: | 51.8770° |
| perigee height: | 468 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 178.3288° |
| argument of perigee: | 60.8650° |
| revolutions per day: | 15.28983199 |
| mean anomaly at epoch: | 299.3956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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