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 43250U 26145.49240057 +.00000000 +00000-0 +60874-5 0 00006
2 43250 86.3938 299.8603 0002217 94.0036 266.1414 14.34217840 02
| Epoch (UTC): | 25 May 2026 11:49:03 |
| Eccentricity: | 0.0002217 |
| inclination: | 86.3938° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 299.8603° |
| argument of perigee: | 94.0036° |
| revolutions per day: | 14.34217840 |
| mean anomaly at epoch: | 266.1414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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