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 24971U 26105.46879088 +.00000000 +00000-0 +46145-4 0 00004
2 24971 98.8422 98.3117 0053040 53.3617 307.2428 14.35490074 07
| Epoch (UTC): | 15 April 2026 11:15:03 |
| Eccentricity: | 0.0053040 |
| inclination: | 98.8422° |
| perigee height: | 736 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 98.3117° |
| argument of perigee: | 53.3617° |
| revolutions per day: | 14.35490074 |
| mean anomaly at epoch: | 307.2428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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