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 28129U 26145.21299112 +.00000000 +00000-0 +00000-0 0 00000
2 28129 55.0136 24.1172 0002250 336.1752 23.8515 1.92678495 02
| Epoch (UTC): | 25 May 2026 05:06:42 |
| Eccentricity: | 0.0002250 |
| inclination: | 55.0136° |
| perigee height: | 20896 km |
| apogee height: | 20908 km |
| right ascension of ascending node: | 24.1172° |
| argument of perigee: | 336.1752° |
| revolutions per day: | 1.92678495 |
| mean anomaly at epoch: | 23.8515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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