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 61254U 26145.40507317 +.00000000 +00000-0 +14586-4 0 00004
2 61254 53.1590 38.2159 0000783 65.6297 294.4803 15.69712320 00
| Epoch (UTC): | 25 May 2026 09:43:18 |
| Eccentricity: | 0.0000783 |
| inclination: | 53.1590° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 38.2159° |
| argument of perigee: | 65.6297° |
| revolutions per day: | 15.69712320 |
| mean anomaly at epoch: | 294.4803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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