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 65967U 26145.29307052 +.00000000 +00000-0 -23099-3 0 00009
2 65967 51.9053 4.4754 0000996 116.4563 243.6502 14.79930052 04
| Epoch (UTC): | 25 May 2026 07:02:01 |
| Eccentricity: | 0.0000996 |
| inclination: | 51.9053° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 4.4754° |
| argument of perigee: | 116.4563° |
| revolutions per day: | 14.79930052 |
| mean anomaly at epoch: | 243.6502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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