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 28912U 26065.59066247 +.00000000 +00000-0 +00000-0 0 00003
2 28912 9.1298 55.1603 0001600 224.1198 143.4443 1.00278557 05
| Epoch (UTC): | 06 March 2026 14:10:33 |
| Eccentricity: | 0.0001600 |
| inclination: | 9.1298° |
| perigee height: | 35778 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 55.1603° |
| argument of perigee: | 224.1198° |
| revolutions per day: | 1.00278557 |
| mean anomaly at epoch: | 143.4443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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