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 65121U 26145.62822814 +.00000000 +00000-0 +19801-3 0 00001
2 65121 49.9933 278.7085 0020396 334.3750 25.6176 14.83971376 02
| Epoch (UTC): | 25 May 2026 15:04:38 |
| Eccentricity: | 0.0020396 |
| inclination: | 49.9933° |
| perigee height: | 603 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 278.7085° |
| argument of perigee: | 334.3750° |
| revolutions per day: | 14.83971376 |
| mean anomaly at epoch: | 25.6176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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