▸Orbital parameters

Orbit class	SSO
Inclination	97.3775°
Eccentricity	0.0005336
Period	93.2 min
Apogee	435 km
Perigee	428 km
Mean motion	15.44965962 rev/day
RAAN	274.1542°
Arg of perigee	199.4745°
Mean anomaly	160.6301°
B*	3.3188e-4
Rev at epoch	10,546

▸Two-line element set (TLE)

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

1 60526U 24149BL 26187.71560213 .00015557 00000-0 33188-3 0 9997

2 60526 97.3775 274.1542 0005336 199.4745 160.6301 15.44965962105464

▸ source OMM (JSON)

{
  "OBJECT_NAME": "DEIMOS",
  "OBJECT_ID": "2024-149BL",
  "EPOCH": "2026-07-06T17:10:28.024+00:00",
  "MEAN_MOTION": 15.44965962,
  "ECCENTRICITY": 0.0005336,
  "INCLINATION": 97.3775,
  "RA_OF_ASC_NODE": 274.1542,
  "ARG_OF_PERICENTER": 199.4745,
  "MEAN_ANOMALY": 160.6301,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60526,
  "REV_AT_EPOCH": 10546,
  "BSTAR": 0.00033188,
  "MEAN_MOTION_DOT": 0.00015557,
  "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	DEIMOS
Operator	Aethero SpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Aug 16, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2HIGHvia 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/60526

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