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 31573U 26145.47186029 +.00000000 +00000-0 +29454-3 0 00004
2 31573 52.0044 316.4189 0002673 102.1106 285.6120 12.23470544 03
| Epoch (UTC): | 25 May 2026 11:19:28 |
| Eccentricity: | 0.0002673 |
| inclination: | 52.0044° |
| perigee height: | 1575 km |
| apogee height: | 1580 km |
| right ascension of ascending node: | 316.4189° |
| argument of perigee: | 102.1106° |
| revolutions per day: | 12.23470544 |
| mean anomaly at epoch: | 285.6120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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