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 54031U 26143.99626682 +.00000000 +00000-0 +00000-0 0 00000
2 54031 64.2867 315.4211 0012040 176.3040 183.7030 2.13101609 08
| Epoch (UTC): | 23 May 2026 23:54:37 |
| Eccentricity: | 0.0012040 |
| inclination: | 64.2867° |
| perigee height: | 19099 km |
| apogee height: | 19161 km |
| right ascension of ascending node: | 315.4211° |
| argument of perigee: | 176.3040° |
| revolutions per day: | 2.13101609 |
| mean anomaly at epoch: | 183.7030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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