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 46130U 26146.21677521 +.00000000 +00000-0 +10886-2 0 00002
2 46130 53.0174 200.3136 0009342 327.5587 32.4880 16.29673367 01
| Epoch (UTC): | 26 May 2026 05:12:09 |
| Eccentricity: | 0.0009342 |
| inclination: | 53.0174° |
| perigee height: | 187 km |
| apogee height: | 200 km |
| right ascension of ascending node: | 200.3136° |
| argument of perigee: | 327.5587° |
| revolutions per day: | 16.29673367 |
| mean anomaly at epoch: | 32.4880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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