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 52159U 26155.20833920 +.00000000 +00000-0 +12874-3 0 00006
2 52159 97.9793 237.6417 0001395 81.4894 278.6473 14.74977714 08
| Epoch (UTC): | 04 June 2026 05:00:00 |
| Eccentricity: | 0.0001395 |
| inclination: | 97.9793° |
| perigee height: | 644 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 237.6417° |
| argument of perigee: | 81.4894° |
| revolutions per day: | 14.74977714 |
| mean anomaly at epoch: | 278.6473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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