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 12988U 26068.20903801 +.00000000 +00000-0 +64283-4 0 00003
2 12988 82.5252 320.8915 0018643 106.3871 253.9398 14.87266972 01
| Epoch (UTC): | 09 March 2026 05:01:00 |
| Eccentricity: | 0.0018643 |
| inclination: | 82.5252° |
| perigee height: | 593 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 320.8915° |
| argument of perigee: | 106.3871° |
| revolutions per day: | 14.87266972 |
| mean anomaly at epoch: | 253.9398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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