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 52900U 26145.66579838 +.00000000 +00000-0 +11022-3 0 00008
2 52900 98.2232 288.2658 0008943 96.4310 263.7910 14.61814131 08
| Epoch (UTC): | 25 May 2026 15:58:44 |
| Eccentricity: | 0.0008943 |
| inclination: | 98.2232° |
| perigee height: | 681 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 288.2658° |
| argument of perigee: | 96.4310° |
| revolutions per day: | 14.61814131 |
| mean anomaly at epoch: | 263.7910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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