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 15054U 26040.77540800 +.00000000 +00000-0 +18403-2 0 00009
2 15054 51.9724 235.4343 4701946 114.0253 301.4153 6.15256511 05
| Epoch (UTC): | 09 February 2026 18:36:35 |
| Eccentricity: | 0.4701946 |
| inclination: | 51.9724° |
| perigee height: | 287 km |
| apogee height: | 12118 km |
| right ascension of ascending node: | 235.4343° |
| argument of perigee: | 114.0253° |
| revolutions per day: | 6.15256511 |
| mean anomaly at epoch: | 301.4153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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