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 61217U 26145.20565439 +.00000000 +00000-0 -11072-4 0 00008
2 61217 53.1610 327.0211 0001787 86.3587 273.7618 15.30183488 06
| Epoch (UTC): | 25 May 2026 04:56:08 |
| Eccentricity: | 0.0001787 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 327.0211° |
| argument of perigee: | 86.3587° |
| revolutions per day: | 15.30183488 |
| mean anomaly at epoch: | 273.7618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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