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 42964U 26145.43290258 +.00000000 +00000-0 +18844-4 0 00008
2 42964 86.3993 34.8903 0002719 81.9898 278.1606 14.34217702 05
| Epoch (UTC): | 25 May 2026 10:23:22 |
| Eccentricity: | 0.0002719 |
| inclination: | 86.3993° |
| perigee height: | 776 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 34.8903° |
| argument of perigee: | 81.9898° |
| revolutions per day: | 14.34217702 |
| mean anomaly at epoch: | 278.1606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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