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 61870U 26145.64990391 +.00000000 +00000-0 +47007-3 0 00005
2 61870 97.4187 216.0074 0012195 53.2848 306.9511 15.29571543 05
| Epoch (UTC): | 25 May 2026 15:35:51 |
| Eccentricity: | 0.0012195 |
| inclination: | 97.4187° |
| perigee height: | 469 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 216.0074° |
| argument of perigee: | 53.2848° |
| revolutions per day: | 15.29571543 |
| mean anomaly at epoch: | 306.9511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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