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 62874U 26145.40368209 +.00000000 +00000-0 +61743-3 0 00004
2 62874 53.1557 133.4126 0000360 42.8144 317.2885 15.30215413 06
| Epoch (UTC): | 25 May 2026 09:41:18 |
| Eccentricity: | 0.0000360 |
| inclination: | 53.1557° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 133.4126° |
| argument of perigee: | 42.8144° |
| revolutions per day: | 15.30215413 |
| mean anomaly at epoch: | 317.2885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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