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 46494U 26145.59640580 +.00000000 +00000-0 +41837-3 0 00001
2 46494 97.8640 159.5885 0005744 359.5222 0.6020 15.47361576 05
| Epoch (UTC): | 25 May 2026 14:18:49 |
| Eccentricity: | 0.0005744 |
| inclination: | 97.8640° |
| perigee height: | 421 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 159.5885° |
| argument of perigee: | 359.5222° |
| revolutions per day: | 15.47361576 |
| mean anomaly at epoch: | 0.6020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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