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 62598U 26145.04291573 +.00000000 +00000-0 +13887-2 0 00001
2 62598 43.0011 25.8368 0002017 265.6534 94.4103 15.70867065 00
| Epoch (UTC): | 25 May 2026 01:01:47 |
| Eccentricity: | 0.0002017 |
| inclination: | 43.0011° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 25.8368° |
| argument of perigee: | 265.6534° |
| revolutions per day: | 15.70867065 |
| mean anomaly at epoch: | 94.4103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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