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 26039.80049560 +.00000000 +00000-0 +17054-2 0 00009
2 15054 51.9727 236.3503 4702340 113.3576 302.1169 6.15222000 06
| Epoch (UTC): | 08 February 2026 19:12:42 |
| Eccentricity: | 0.4702340 |
| inclination: | 51.9727° |
| perigee height: | 287 km |
| apogee height: | 12119 km |
| right ascension of ascending node: | 236.3503° |
| argument of perigee: | 113.3576° |
| revolutions per day: | 6.15222000 |
| mean anomaly at epoch: | 302.1169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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