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 55012U 26145.44389289 +.00000000 +00000-0 +74387-3 0 00003
2 55012 97.3284 215.7584 0006798 166.7747 193.3684 15.48871963 04
| Epoch (UTC): | 25 May 2026 10:39:12 |
| Eccentricity: | 0.0006798 |
| inclination: | 97.3284° |
| perigee height: | 415 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 215.7584° |
| argument of perigee: | 166.7747° |
| revolutions per day: | 15.48871963 |
| mean anomaly at epoch: | 193.3684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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