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 62919U 26145.54746414 +.00000000 +00000-0 +13353-2 0 00000
2 62919 42.9989 244.0470 0002539 260.1537 99.9044 15.70913992 05
| Epoch (UTC): | 25 May 2026 13:08:20 |
| Eccentricity: | 0.0002539 |
| inclination: | 42.9989° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 244.0470° |
| argument of perigee: | 260.1537° |
| revolutions per day: | 15.70913992 |
| mean anomaly at epoch: | 99.9044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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