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 20026U 26145.52079332 +.00000000 +00000-0 +00000-0 0 00002
2 20026 64.9496 311.3160 0020620 212.5971 152.7735 2.13204601 01
| Epoch (UTC): | 25 May 2026 12:29:56 |
| Eccentricity: | 0.0020620 |
| inclination: | 64.9496° |
| perigee height: | 19069 km |
| apogee height: | 19174 km |
| right ascension of ascending node: | 311.3160° |
| argument of perigee: | 212.5971° |
| revolutions per day: | 2.13204601 |
| mean anomaly at epoch: | 152.7735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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