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 46912U 26145.58627852 +.00000000 +00000-0 +27731-3 0 00009
2 46912 36.8947 200.6566 0002507 156.0621 204.0244 15.25559964 08
| Epoch (UTC): | 25 May 2026 14:04:14 |
| Eccentricity: | 0.0002507 |
| inclination: | 36.8947° |
| perigee height: | 487 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 200.6566° |
| argument of perigee: | 156.0621° |
| revolutions per day: | 15.25559964 |
| mean anomaly at epoch: | 204.0244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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