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 64121U 26145.40341477 +.00000000 +00000-0 +57867-3 0 00001
2 64121 53.1621 30.7178 0001355 79.4123 280.7030 15.30219546 06
| Epoch (UTC): | 25 May 2026 09:40:55 |
| Eccentricity: | 0.0001355 |
| inclination: | 53.1621° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 30.7178° |
| argument of perigee: | 79.4123° |
| revolutions per day: | 15.30219546 |
| mean anomaly at epoch: | 280.7030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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