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 65948U 26145.38087678 +.00000000 +00000-0 +31333-3 0 00006
2 65948 51.8988 16.4531 0000936 102.3928 257.7139 14.79935360 07
| Epoch (UTC): | 25 May 2026 09:08:27 |
| Eccentricity: | 0.0000936 |
| inclination: | 51.8988° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 16.4531° |
| argument of perigee: | 102.3928° |
| revolutions per day: | 14.79935360 |
| mean anomaly at epoch: | 257.7139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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