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 42987U 26145.37438157 +.00000000 +00000-0 +38368-3 0 00000
2 42987 97.4325 293.2390 0001608 104.3290 255.8143 15.56572534 05
| Epoch (UTC): | 25 May 2026 08:59:06 |
| Eccentricity: | 0.0001608 |
| inclination: | 97.4325° |
| perigee height: | 396 km |
| apogee height: | 399 km |
| right ascension of ascending node: | 293.2390° |
| argument of perigee: | 104.3290° |
| revolutions per day: | 15.56572534 |
| mean anomaly at epoch: | 255.8143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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