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 61874U 26145.56182916 +.00000000 +00000-0 +13136-4 0 00003
2 61874 53.1601 337.6727 0000518 109.4501 250.6573 15.69709084 00
| Epoch (UTC): | 25 May 2026 13:29:02 |
| Eccentricity: | 0.0000518 |
| inclination: | 53.1601° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 337.6727° |
| argument of perigee: | 109.4501° |
| revolutions per day: | 15.69709084 |
| mean anomaly at epoch: | 250.6573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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