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 62870U 26145.28439779 +.00000000 +00000-0 +71813-3 0 00006
2 62870 53.1605 132.6733 0001038 91.6959 268.4163 15.34404996 06
| Epoch (UTC): | 25 May 2026 06:49:31 |
| Eccentricity: | 0.0001038 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 132.6733° |
| argument of perigee: | 91.6959° |
| revolutions per day: | 15.34404996 |
| mean anomaly at epoch: | 268.4163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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