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 26065.94722299 +.00000000 +00000-0 +91200-4 0 00005
2 24971 98.8394 57.8164 0052323 167.8146 192.4317 14.35468322 00
| Epoch (UTC): | 06 March 2026 22:44:00 |
| Eccentricity: | 0.0052323 |
| inclination: | 98.8394° |
| perigee height: | 736 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 57.8164° |
| argument of perigee: | 167.8146° |
| revolutions per day: | 14.35468322 |
| mean anomaly at epoch: | 192.4317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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