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 26140.92566542 +.00000000 +00000-0 +83401-4 0 00007
2 00020 33.3579 5.0875 1638376 267.4436 73.8409 11.61950661 02
| Epoch (UTC): | 20 May 2026 22:12:57 |
| Eccentricity: | 0.1638376 |
| inclination: | 33.3579° |
| perigee height: | 507 km |
| apogee height: | 3205 km |
| right ascension of ascending node: | 5.0875° |
| argument of perigee: | 267.4436° |
| revolutions per day: | 11.61950661 |
| mean anomaly at epoch: | 73.8409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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