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 65123U 26145.58593654 +.00000000 +00000-0 +18313-3 0 00002
2 65123 49.9948 233.0658 0008246 234.6044 125.4123 14.82054690 09
| Epoch (UTC): | 25 May 2026 14:03:44 |
| Eccentricity: | 0.0008246 |
| inclination: | 49.9948° |
| perigee height: | 617 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 233.0658° |
| argument of perigee: | 234.6044° |
| revolutions per day: | 14.82054690 |
| mean anomaly at epoch: | 125.4123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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