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 43187U 26053.69582773 +.00000000 +00000-0 +36084-3 0 00003
2 43187 97.5451 319.2311 0010661 56.3278 303.8970 15.15376127 09
| Epoch (UTC): | 22 February 2026 16:41:59 |
| Eccentricity: | 0.0010661 |
| inclination: | 97.5451° |
| perigee height: | 512 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 319.2311° |
| argument of perigee: | 56.3278° |
| revolutions per day: | 15.15376127 |
| mean anomaly at epoch: | 303.8970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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