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 29486U 26145.13829324 +.00000000 +00000-0 +00000-0 0 00002
2 29486 54.7074 152.2538 0106241 53.9126 3.0347 2.00571164 07
| Epoch (UTC): | 25 May 2026 03:19:08 |
| Eccentricity: | 0.0106241 |
| inclination: | 54.7074° |
| perigee height: | 19899 km |
| apogee height: | 20464 km |
| right ascension of ascending node: | 152.2538° |
| argument of perigee: | 53.9126° |
| revolutions per day: | 2.00571164 |
| mean anomaly at epoch: | 3.0347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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