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 25134U 26103.47839977 +.00000000 +00000-0 +00000-0 0 00004
2 25134 12.7687 11.1754 0002465 183.7444 342.9475 0.99157075 02
| Epoch (UTC): | 13 April 2026 11:28:53 |
| Eccentricity: | 0.0002465 |
| inclination: | 12.7687° |
| perigee height: | 36092 km |
| apogee height: | 36112 km |
| right ascension of ascending node: | 11.1754° |
| argument of perigee: | 183.7444° |
| revolutions per day: | 0.99157075 |
| mean anomaly at epoch: | 342.9475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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