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 62174U 26145.23412750 +.00000000 +00000-0 +16943-3 0 00001
2 62174 70.0010 331.3427 0002894 272.5412 87.5416 14.98364776 05
| Epoch (UTC): | 25 May 2026 05:37:08 |
| Eccentricity: | 0.0002894 |
| inclination: | 70.0010° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 331.3427° |
| argument of perigee: | 272.5412° |
| revolutions per day: | 14.98364776 |
| mean anomaly at epoch: | 87.5416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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