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 61257U 26145.43808299 +.00000000 +00000-0 +18656-3 0 00004
2 61257 53.1602 197.5875 0000900 74.8561 285.2539 15.30243170 02
| Epoch (UTC): | 25 May 2026 10:30:50 |
| Eccentricity: | 0.0000900 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 197.5875° |
| argument of perigee: | 74.8561° |
| revolutions per day: | 15.30243170 |
| mean anomaly at epoch: | 285.2539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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