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 25118U 26087.68697353 +.00000000 +00000-0 +48281-3 0 00006
2 25118 45.0140 80.1792 0002714 274.6610 255.2153 14.47335555 05
| Epoch (UTC): | 28 March 2026 16:29:14 |
| Eccentricity: | 0.0002714 |
| inclination: | 45.0140° |
| perigee height: | 732 km |
| apogee height: | 736 km |
| right ascension of ascending node: | 80.1792° |
| argument of perigee: | 274.6610° |
| revolutions per day: | 14.47335555 |
| mean anomaly at epoch: | 255.2153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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