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 61672U 26145.27342795 +.00000000 +00000-0 +31878-3 0 00002
2 61672 53.1581 95.1631 0001201 83.7128 276.4010 15.30219663 01
| Epoch (UTC): | 25 May 2026 06:33:44 |
| Eccentricity: | 0.0001201 |
| inclination: | 53.1581° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.1631° |
| argument of perigee: | 83.7128° |
| revolutions per day: | 15.30219663 |
| mean anomaly at epoch: | 276.4010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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