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N2-P-BODY, 69929

Orbit data source: Space-Track

N2-P-BODY, 69929 is an American payload satellite in SSO that was launched on Tue, 07 Jul 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Iframe URL

https://www.satcat.com/sats-embedded/69929?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

69929, 2026-156BN

Orbit

SSO

Country

Related business

NOVI LLC (US)

Manufacturer

NOVI

Mission

Operational spacecraft

Bus & Motor

CUBESAT 6U, Unknown motor

Mass

13 kg wet, 13 kg dry

Launch date (UTC)

2026-07-07 (1 month ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

BOX+ 2 PAN, 1.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago

0 N2-P-BODY
1 69929U 26156BN  26227.29671745  .00002112  00000-0  21095-3 0  9991
2 69929  97.7510 127.1524 0010058  37.8193 322.3731 14.92524207  5814

Epoch: 2026-08-15T07:07Z

TLE epoch observation values (Epoch: 2026-08-15T07:07:16.387Z)

Latitude

-0.00005°

Longitude

56.6245°

Altitude

587.562 km

Speed

7.569 km/s

True Right ascension

08h 28m 36s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

12:50:01

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

594.091 km

Perigee altitude

580.08 km

Semi-major axis

6,965.222 km

Eccentricity

0.00101

Inclination

97.751°

RAAN

127.1524°

Arg. of periapsis

37.8193°

True anomaly

322.30266°

Mean anomaly

322.3731°

Eccentric anomaly

322.33789°

Mean motion

3.73371 °/min

Orbital period

96.42 mins

BSTAR

0.00021095

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Other satellites on launch #156 in the year 2026 (2026-07-07 UTC)

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N2-P-BODY Visibility forecast

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Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
8 mins	2026-08-16 06:12:10.866Z	14.447° NNE	2026-08-16 06:16:10.866Z	83.617° E	44.604°	2026-08-16 06:20:10.866Z	189.993° SSW
6 mins	2026-08-16 17:03:10.866Z	139.234° SSE	2026-08-16 17:06:10.866Z	49.32° ENE	35.275°	2026-08-16 17:09:10.866Z	1.382° NNE

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out N2-P-BODY, 69929 on other resources

View N2-P-BODY, 69929 on NASA - NSSDCA Website

View N2-P-BODY, 69929 on Heavens-Above

View N2-P-BODY, 69929 on Keep Track

View N2-P-BODY, 69929 on Celestrak

View N2-P-BODY, 69929 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

N2-P-BODY, 69929

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2026-08-15T07:07:16.387Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #156 in the year 2026 (2026-07-07 UTC)

N2-P-BODY Visibility forecast

Co-orbital & Co-planar RSOs

Check out N2-P-BODY, 69929 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 15 hours ago