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 62080U 26145.40144380 +.00000000 +00000-0 +13646-4 0 00005
2 62080 97.4393 153.0618 0001290 113.1506 246.9865 15.19719372 01
| Epoch (UTC): | 25 May 2026 09:38:04 |
| Eccentricity: | 0.0001290 |
| inclination: | 97.4393° |
| perigee height: | 506 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 153.0618° |
| argument of perigee: | 113.1506° |
| revolutions per day: | 15.19719372 |
| mean anomaly at epoch: | 246.9865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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