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 43778U 26145.06086251 +.00000000 +00000-0 +36930-3 0 00002
2 43778 97.3812 193.6965 0012487 45.9705 314.2559 15.22872121 02
| Epoch (UTC): | 25 May 2026 01:27:38 |
| Eccentricity: | 0.0012487 |
| inclination: | 97.3812° |
| perigee height: | 489 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 193.6965° |
| argument of perigee: | 45.9705° |
| revolutions per day: | 15.22872121 |
| mean anomaly at epoch: | 314.2559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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