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 43687U 26145.18750412 +.00000000 +00000-0 +00000-0 0 00007
2 43687 64.2931 193.3710 0011484 256.0033 103.9404 2.13102011 08
| Epoch (UTC): | 25 May 2026 04:30:00 |
| Eccentricity: | 0.0011484 |
| inclination: | 64.2931° |
| perigee height: | 19101 km |
| apogee height: | 19159 km |
| right ascension of ascending node: | 193.3710° |
| argument of perigee: | 256.0033° |
| revolutions per day: | 2.13102011 |
| mean anomaly at epoch: | 103.9404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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