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 46809U 26145.61284860 +.00000000 +00000-0 +15296-3 0 00009
2 46809 34.9955 228.4558 0006960 235.9187 124.0861 15.02560996 09
| Epoch (UTC): | 25 May 2026 14:42:30 |
| Eccentricity: | 0.0006960 |
| inclination: | 34.9955° |
| perigee height: | 554 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 228.4558° |
| argument of perigee: | 235.9187° |
| revolutions per day: | 15.02560996 |
| mean anomaly at epoch: | 124.0861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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