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 62909U 26145.34091214 +.00000000 +00000-0 +14586-2 0 00007
2 62909 43.0000 245.9699 0002395 262.0958 97.9638 15.70954427 06
| Epoch (UTC): | 25 May 2026 08:10:54 |
| Eccentricity: | 0.0002395 |
| inclination: | 43.0000° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 245.9699° |
| argument of perigee: | 262.0958° |
| revolutions per day: | 15.70954427 |
| mean anomaly at epoch: | 97.9638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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