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 26069.50211242 +.00000000 +00000-0 +10203-3 0 00005
2 24971 98.8398 61.4579 0052500 157.4003 202.9510 14.35470535 00
| Epoch (UTC): | 10 March 2026 12:03:02 |
| Eccentricity: | 0.0052500 |
| inclination: | 98.8398° |
| perigee height: | 736 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 61.4579° |
| argument of perigee: | 157.4003° |
| revolutions per day: | 14.35470535 |
| mean anomaly at epoch: | 202.9510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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