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 02874U 26145.35156122 +.00000000 +00000-0 +49830-4 0 00005
2 02874 69.9717 164.2530 0009581 237.1634 122.8550 13.96824648 06
| Epoch (UTC): | 25 May 2026 08:26:14 |
| Eccentricity: | 0.0009581 |
| inclination: | 69.9717° |
| perigee height: | 898 km |
| apogee height: | 912 km |
| right ascension of ascending node: | 164.2530° |
| argument of perigee: | 237.1634° |
| revolutions per day: | 13.96824648 |
| mean anomaly at epoch: | 122.8550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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