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 61008U 26145.07642767 +.00000000 +00000-0 -38875-4 0 00001
2 61008 53.1602 70.8445 0001265 91.5017 268.6128 15.30197937 07
| Epoch (UTC): | 25 May 2026 01:50:03 |
| Eccentricity: | 0.0001265 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 70.8445° |
| argument of perigee: | 91.5017° |
| revolutions per day: | 15.30197937 |
| mean anomaly at epoch: | 268.6128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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