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 57623U 26145.30668262 +.00000000 +00000-0 -67455-4 0 00009
2 57623 43.0028 8.9126 0001008 259.2867 100.7871 15.27580802 08
| Epoch (UTC): | 25 May 2026 07:21:37 |
| Eccentricity: | 0.0001008 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.9126° |
| argument of perigee: | 259.2867° |
| revolutions per day: | 15.27580802 |
| mean anomaly at epoch: | 100.7871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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