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 62839U 26145.58335647 +.00000000 +00000-0 +11589-3 0 00007
2 62839 43.0011 202.8723 0001553 269.4602 315.2770 15.70819312 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001553 |
| inclination: | 43.0011° |
| perigee height: | 356 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 202.8723° |
| argument of perigee: | 269.4602° |
| revolutions per day: | 15.70819312 |
| mean anomaly at epoch: | 315.2770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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