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 26087.99223817 +.00000000 +00000-0 +84429-4 0 00009
2 02874 69.9726 287.1974 0009738 291.5226 68.4841 13.96815735 03
| Epoch (UTC): | 28 March 2026 23:48:49 |
| Eccentricity: | 0.0009738 |
| inclination: | 69.9726° |
| perigee height: | 898 km |
| apogee height: | 912 km |
| right ascension of ascending node: | 287.1974° |
| argument of perigee: | 291.5226° |
| revolutions per day: | 13.96815735 |
| mean anomaly at epoch: | 68.4841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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