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 46791C 20074BE 25043.03451389 .10025000 00000+0 19347-2 0 430
2 46791 53.0252 225.8026 0012910 288.8536 303.0552 16.30665817 16
| Epoch (UTC): | 12 February 2025 00:49:42 |
| Eccentricity: | 0.0012910 |
| inclination: | 53.0252° |
| perigee height: | 182 km |
| apogee height: | 199 km |
| right ascension of ascending node: | 225.8026° |
| argument of perigee: | 288.8536° |
| revolutions per day: | 16.30665817 |
| mean anomaly at epoch: | 303.0552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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