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 62288U 26145.46047271 +.00000000 +00000-0 +57283-3 0 00006
2 62288 42.9997 131.4983 0001036 279.4136 80.6599 15.27587660 03
| Epoch (UTC): | 25 May 2026 11:03:04 |
| Eccentricity: | 0.0001036 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 131.4983° |
| argument of perigee: | 279.4136° |
| revolutions per day: | 15.27587660 |
| mean anomaly at epoch: | 80.6599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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