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 26464U 26143.67364213 +.00000000 +00000-0 +00000-0 0 00003
2 26464 150.1185 47.6077 9031581 264.3140 3.6732 0.44403233 07
| Epoch (UTC): | 23 May 2026 16:10:02 |
| Eccentricity: | 0.9031581 |
| inclination: | 150.1185° |
| perigee height: | 650 km |
| apogee height: | 131745 km |
| right ascension of ascending node: | 47.6077° |
| argument of perigee: | 264.3140° |
| revolutions per day: | 0.44403233 |
| mean anomaly at epoch: | 3.6732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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