▸Orbital parameters

Orbit class	SSO
Inclination	97.7022°
Eccentricity	0.0005334
Period	92.6 min
Apogee	404 km
Perigee	396 km
Mean motion	15.55788133 rev/day
RAAN	22.9295°
Arg of perigee	268.1980°
Mean anomaly	91.8662°
B*	2.2487e-4
Rev at epoch	28,038

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 48951U 21059CA 26187.99233347 .00015424 00000-0 22487-3 0 9990

2 48951 97.7022 22.9295 0005334 268.1980 91.8662 15.55788133280383

▸ source OMM (JSON)

{
  "OBJECT_NAME": "DEMO8 (TENZING)",
  "OBJECT_ID": "2021-059CA",
  "EPOCH": "2026-07-06T23:48:57.612+00:00",
  "MEAN_MOTION": 15.55788133,
  "ECCENTRICITY": 0.0005334,
  "INCLINATION": 97.7022,
  "RA_OF_ASC_NODE": 22.9295,
  "ARG_OF_PERICENTER": 268.198,
  "MEAN_ANOMALY": 91.8662,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 48951,
  "REV_AT_EPOCH": 28038,
  "BSTAR": 0.00022487,
  "MEAN_MOTION_DOT": 0.00015424,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	DEMO8 (TENZING)
Operator	Astro Digital / Orbit FabHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jun 30, 2021HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	35HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/48951

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.