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 25394U 26142.30806726 +.00000000 +00000-0 +52040-4 0 00008
2 25394 98.9415 115.3904 0001330 158.3565 201.7670 14.25115992 06
| Epoch (UTC): | 22 May 2026 07:23:37 |
| Eccentricity: | 0.0001330 |
| inclination: | 98.9415° |
| perigee height: | 807 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 115.3904° |
| argument of perigee: | 158.3565° |
| revolutions per day: | 14.25115992 |
| mean anomaly at epoch: | 201.7670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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