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 00020U 26073.79543251 +.00000000 +00000-0 +34117-3 0 00008
2 00020 33.3531 246.7874 1638552 267.5238 73.7607 11.61878020 07
| Epoch (UTC): | 14 March 2026 19:05:25 |
| Eccentricity: | 0.1638552 |
| inclination: | 33.3531° |
| perigee height: | 507 km |
| apogee height: | 3205 km |
| right ascension of ascending node: | 246.7874° |
| argument of perigee: | 267.5238° |
| revolutions per day: | 11.61878020 |
| mean anomaly at epoch: | 73.7607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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