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 62840U 26145.57540139 +.00000000 +00000-0 +12382-2 0 00003
2 62840 43.0009 202.4720 0001788 258.9652 101.1015 15.70877987 04
| Epoch (UTC): | 25 May 2026 13:48:34 |
| Eccentricity: | 0.0001788 |
| inclination: | 43.0009° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 202.4720° |
| argument of perigee: | 258.9652° |
| revolutions per day: | 15.70877987 |
| mean anomaly at epoch: | 101.1015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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