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 65120U 26145.66185597 +.00000000 +00000-0 +19504-3 0 00004
2 65120 49.9863 278.7334 0009547 0.8341 359.2612 14.83888511 05
| Epoch (UTC): | 25 May 2026 15:53:04 |
| Eccentricity: | 0.0009547 |
| inclination: | 49.9863° |
| perigee height: | 610 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 278.7334° |
| argument of perigee: | 0.8341° |
| revolutions per day: | 14.83888511 |
| mean anomaly at epoch: | 359.2612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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