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 61894U 26145.60958750 +.00000000 +00000-0 +45843-3 0 00006
2 61894 97.4136 216.3672 0015446 230.9728 129.0128 15.11517038 03
| Epoch (UTC): | 25 May 2026 14:37:48 |
| Eccentricity: | 0.0015446 |
| inclination: | 97.4136° |
| perigee height: | 521 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 216.3672° |
| argument of perigee: | 230.9728° |
| revolutions per day: | 15.11517038 |
| mean anomaly at epoch: | 129.0128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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